9 changed files with 597 additions and 4 deletions
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|
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/****************************************************************************
|
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* |
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* Copyright (c) 2021 PX4 Development Team. All rights reserved. |
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* |
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* Redistribution and use in source and binary forms, with or without |
||||
* modification, are permitted provided that the following conditions |
||||
* are met: |
||||
* |
||||
* 1. Redistributions of source code must retain the above copyright |
||||
* notice, this list of conditions and the following disclaimer. |
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* 2. Redistributions in binary form must reproduce the above copyright |
||||
* notice, this list of conditions and the following disclaimer in |
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* the documentation and/or other materials provided with the |
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* distribution. |
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* 3. Neither the name PX4 nor the names of its contributors may be |
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* used to endorse or promote products derived from this software |
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* without specific prior written permission. |
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* |
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS |
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT |
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS |
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE |
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, |
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, |
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS |
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED |
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT |
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN |
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
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* POSSIBILITY OF SUCH DAMAGE. |
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* |
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****************************************************************************/ |
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#include "autopilot_tester_failure.h" |
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#include "math_helpers.h" |
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#include <iostream> |
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#include <future> |
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#include <thread> |
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#include <unistd.h> |
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void AutopilotTesterFailure::connect(const std::string uri) |
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{ |
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AutopilotTester::connect(uri); |
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auto system = get_system(); |
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_failure.reset(new Failure(system)); |
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} |
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void AutopilotTesterFailure::set_param_sys_failure_en(bool value) |
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{ |
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CHECK(getParams()->set_param_int("SYS_FAILURE_EN", value) == Param::Result::Success); |
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} |
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void AutopilotTesterFailure::set_param_fd_act_en(bool value) |
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{ |
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CHECK(getParams()->set_param_int("FD_ACT_EN", value) == Param::Result::Success); |
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} |
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void AutopilotTesterFailure::set_param_mc_airmode(int value) |
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{ |
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CHECK(getParams()->set_param_int("MC_AIRMODE", value) == Param::Result::Success); |
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} |
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void AutopilotTesterFailure::set_param_ca_failure_mode(int value) |
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{ |
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CHECK(getParams()->set_param_int("CA_FAILURE_MODE", value) == Param::Result::Success); |
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} |
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void AutopilotTesterFailure::set_param_com_act_fail_act(int value) |
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{ |
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CHECK(getParams()->set_param_int("COM_ACT_FAIL_ACT", value) == Param::Result::Success); |
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} |
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void AutopilotTesterFailure::inject_failure(mavsdk::Failure::FailureUnit failure_unit, |
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mavsdk::Failure::FailureType failure_type, int instance, mavsdk::Failure::Result expected_result) |
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{ |
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CHECK(_failure->inject(failure_unit, failure_type, instance) == expected_result); |
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} |
@ -0,0 +1,61 @@
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/****************************************************************************
|
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* |
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* Copyright (c) 2021 PX4 Development Team. All rights reserved. |
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* |
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* Redistribution and use in source and binary forms, with or without |
||||
* modification, are permitted provided that the following conditions |
||||
* are met: |
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* |
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* 1. Redistributions of source code must retain the above copyright |
||||
* notice, this list of conditions and the following disclaimer. |
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* 2. Redistributions in binary form must reproduce the above copyright |
||||
* notice, this list of conditions and the following disclaimer in |
||||
* the documentation and/or other materials provided with the |
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* distribution. |
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* 3. Neither the name PX4 nor the names of its contributors may be |
||||
* used to endorse or promote products derived from this software |
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* without specific prior written permission. |
||||
* |
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS |
||||
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT |
||||
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS |
||||
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE |
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, |
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, |
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS |
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED |
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT |
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN |
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
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* POSSIBILITY OF SUCH DAMAGE. |
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* |
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****************************************************************************/ |
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#pragma once |
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#include "autopilot_tester.h" |
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#include <mavsdk/mavsdk.h> |
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#include <mavsdk/plugins/action/action.h> |
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#include <mavsdk/plugins/failure/failure.h> |
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class AutopilotTesterFailure : public AutopilotTester |
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{ |
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public: |
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AutopilotTesterFailure() = default; |
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~AutopilotTesterFailure() = default; |
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void set_param_sys_failure_en(bool value); |
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void set_param_fd_act_en(bool value); |
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void set_param_mc_airmode(int value); |
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void set_param_ca_failure_mode(int value); |
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void set_param_com_act_fail_act(int value); |
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void inject_failure(mavsdk::Failure::FailureUnit failure_unit, mavsdk::Failure::FailureType failure_type, int instance, |
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mavsdk::Failure::Result expected_result); |
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void connect(const std::string uri); |
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private: |
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std::unique_ptr<mavsdk::Failure> _failure{}; |
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}; |
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/****************************************************************************
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* |
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* Copyright (c) 2021 PX4 Development Team. All rights reserved. |
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* |
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* Redistribution and use in source and binary forms, with or without |
||||
* modification, are permitted provided that the following conditions |
||||
* are met: |
||||
* |
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* 1. Redistributions of source code must retain the above copyright |
||||
* notice, this list of conditions and the following disclaimer. |
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* 2. Redistributions in binary form must reproduce the above copyright |
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* notice, this list of conditions and the following disclaimer in |
||||
* the documentation and/or other materials provided with the |
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* distribution. |
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* 3. Neither the name PX4 nor the names of its contributors may be |
||||
* used to endorse or promote products derived from this software |
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* without specific prior written permission. |
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* |
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS |
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT |
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS |
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE |
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, |
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, |
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS |
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED |
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT |
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN |
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
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* POSSIBILITY OF SUCH DAMAGE. |
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* |
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****************************************************************************/ |
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#include <thread> |
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#include <chrono> |
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#include <math.h> |
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#include "autopilot_tester_failure.h" |
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TEST_CASE("Control Allocation - Remove one motor", "[controlallocation]") |
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{ |
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const float flight_altitude = 10.0f; |
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const float altitude_tolerance = 4.0f; |
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const float hover_speed_tolerance = 1.0f; |
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AutopilotTester::MissionOptions mission_options; |
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mission_options.rtl_at_end = false; |
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mission_options.relative_altitude_m = flight_altitude; |
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AutopilotTesterFailure tester; |
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tester.connect(connection_url); |
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tester.wait_until_ready(); |
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// Configuration
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tester.set_param_sys_failure_en(true); // Enable failure injection
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tester.set_param_fd_act_en(true); // Enable motor failure detection
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tester.set_param_mc_airmode(1); // Enable airmode for control allocation with motor failure
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tester.set_param_ca_failure_mode(1); // Enable control allocation handling of failed motor
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tester.prepare_square_mission(mission_options); |
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tester.set_takeoff_altitude(flight_altitude); |
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tester.set_rtl_altitude(flight_altitude); |
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tester.check_tracks_mission(5.f); |
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tester.store_home(); |
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std::this_thread::sleep_for(std::chrono::seconds( |
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1)); // This is necessary for the takeoff altitude to be applied properly
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// Takeoff
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tester.arm(); |
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tester.takeoff(); |
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tester.wait_until_hovering(); |
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tester.wait_until_altitude(flight_altitude, std::chrono::seconds(30)); |
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tester.wait_until_speed_lower_than(hover_speed_tolerance, std::chrono::seconds(30)); |
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// Motor failure mid-air
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tester.start_checking_altitude(altitude_tolerance); |
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const int motor_instance = 1; |
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tester.inject_failure(mavsdk::Failure::FailureUnit::SystemMotor, mavsdk::Failure::FailureType::Off, motor_instance, |
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mavsdk::Failure::Result::Success); |
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std::this_thread::sleep_for(std::chrono::seconds(1)); |
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tester.execute_mission(); |
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tester.stop_checking_altitude(); |
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// RTL
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tester.execute_rtl(); |
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std::chrono::seconds until_disarmed_timeout = std::chrono::seconds(180); |
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tester.wait_until_disarmed(until_disarmed_timeout); |
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tester.check_home_within(5.f); |
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} |
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TEST_CASE("Control Allocation - Remove two motors", "[controlallocation]") |
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{ |
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const float flight_altitude = 10.0f; |
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const float altitude_tolerance = 4.0f; |
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const float hover_speed_tolerance = 1.0f; |
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AutopilotTesterFailure tester; |
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tester.connect(connection_url); |
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tester.wait_until_ready(); |
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tester.set_param_sys_failure_en(true); // Enable failure injection
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tester.set_param_fd_act_en(true); // Enable motor failure detection
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tester.set_param_mc_airmode(1); // Enable airmode for control allocation with motor failure
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tester.set_param_ca_failure_mode(1); // Enable control allocation handling of failed motor
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AutopilotTester::MissionOptions mission_options; |
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mission_options.rtl_at_end = false; |
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mission_options.relative_altitude_m = flight_altitude; |
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tester.prepare_square_mission(mission_options); |
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tester.set_takeoff_altitude(flight_altitude); |
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tester.set_rtl_altitude(flight_altitude); |
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tester.check_tracks_mission(5.f); |
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tester.store_home(); |
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std::this_thread::sleep_for(std::chrono::seconds( |
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1)); // This is necessary for the takeoff altitude to be applied properly
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tester.arm(); |
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tester.takeoff(); |
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tester.wait_until_hovering(); |
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tester.wait_until_altitude(flight_altitude, std::chrono::seconds(30)); |
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tester.wait_until_speed_lower_than(hover_speed_tolerance, std::chrono::seconds(30)); |
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// Remove two motors opposite of one another on the hexa airframe
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const int first_motor_instance = 1; |
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const int second_motor_instance = 2; |
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tester.start_checking_altitude(altitude_tolerance); |
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tester.inject_failure(mavsdk::Failure::FailureUnit::SystemMotor, mavsdk::Failure::FailureType::Off, |
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first_motor_instance, |
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mavsdk::Failure::Result::Success); |
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std::this_thread::sleep_for(std::chrono::seconds(1)); |
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tester.inject_failure(mavsdk::Failure::FailureUnit::SystemMotor, mavsdk::Failure::FailureType::Off, |
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second_motor_instance, |
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mavsdk::Failure::Result::Success); |
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std::this_thread::sleep_for(std::chrono::seconds(1)); |
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tester.execute_mission(); |
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tester.stop_checking_altitude(); |
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// RTL with two motors out won't work because navigator will wait forever until
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// the yaw setpoint is reached during RTL, and it won't land.
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tester.land(); |
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std::chrono::seconds until_disarmed_timeout = std::chrono::seconds(180); |
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tester.wait_until_disarmed(until_disarmed_timeout); |
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} |
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TEST_CASE("Control Allocation - Remove and restore every motor once", "[controlallocation]") |
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{ |
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const float flight_altitude = 10.0f; |
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const float altitude_tolerance = 4.0f; |
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const float hover_speed_tolerance = 1.0f; |
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AutopilotTesterFailure tester; |
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tester.connect(connection_url); |
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tester.wait_until_ready(); |
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tester.set_param_sys_failure_en(true); // Enable failure injection
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tester.set_param_fd_act_en(true); // Enable motor failure detection
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tester.set_param_mc_airmode(1); // Enable airmode for control allocation with motor failure
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tester.set_param_ca_failure_mode(1); // Enable control allocation handling of failed motor
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AutopilotTester::MissionOptions mission_options; |
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mission_options.rtl_at_end = false; |
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mission_options.relative_altitude_m = flight_altitude; |
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tester.prepare_square_mission(mission_options); |
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tester.set_takeoff_altitude(flight_altitude); |
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tester.set_rtl_altitude(flight_altitude); |
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tester.check_tracks_mission(5.f); |
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tester.store_home(); |
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std::this_thread::sleep_for(std::chrono::seconds( |
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1)); // This is necessary for the takeoff altitude to be applied properly
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tester.arm(); |
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tester.takeoff(); |
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tester.wait_until_hovering(); |
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tester.wait_until_altitude(flight_altitude, std::chrono::seconds(30)); |
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tester.wait_until_speed_lower_than(hover_speed_tolerance, std::chrono::seconds(30)); |
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tester.start_checking_altitude(altitude_tolerance); |
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for (int m = 1; m <= 6; m++) { |
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tester.inject_failure(mavsdk::Failure::FailureUnit::SystemMotor, mavsdk::Failure::FailureType::Off, m, |
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mavsdk::Failure::Result::Success); |
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std::this_thread::sleep_for(std::chrono::seconds(1)); |
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tester.inject_failure(mavsdk::Failure::FailureUnit::SystemMotor, mavsdk::Failure::FailureType::Ok, m, |
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mavsdk::Failure::Result::Success); |
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std::this_thread::sleep_for(std::chrono::seconds(1)); |
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} |
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tester.execute_mission(); |
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tester.stop_checking_altitude(); |
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tester.execute_rtl(); |
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std::chrono::seconds until_disarmed_timeout = std::chrono::seconds(180); |
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tester.wait_until_disarmed(until_disarmed_timeout); |
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tester.check_home_within(5.f); |
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} |
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TEST_CASE("Control Allocation - Return home on motor failure", "[controlallocation]") |
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{ |
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const float flight_altitude = 10.0f; |
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const float hover_speed_tolerance = 1.0f; |
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AutopilotTesterFailure tester; |
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tester.connect(connection_url); |
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tester.wait_until_ready(); |
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// Configuration
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tester.set_param_sys_failure_en(true); // Enable failure injection
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tester.set_param_fd_act_en(true); // Enable motor failure detection
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tester.set_param_mc_airmode(1); // Enable airmode for control allocation with motor failure
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tester.set_param_ca_failure_mode(1); // Enable control allocation handling of failed motor
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tester.set_param_com_act_fail_act(3); // RTL on motor failure
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tester.set_takeoff_altitude(flight_altitude); |
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tester.store_home(); |
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std::this_thread::sleep_for(std::chrono::seconds( |
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1)); // This is necessary for the takeoff altitude to be applied properly
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// Takeoff
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tester.arm(); |
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tester.takeoff(); |
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tester.wait_until_hovering(); |
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tester.wait_until_altitude(flight_altitude, std::chrono::seconds(30)); |
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tester.wait_until_speed_lower_than(hover_speed_tolerance, std::chrono::seconds(30)); |
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// TODO: Minor improvement, fly forward for a little bit before triggering motor failure to distinguish "RTL" and "Land only"
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// Motor failure mid-air
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const int motor_instance = 1; |
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tester.inject_failure(mavsdk::Failure::FailureUnit::SystemMotor, mavsdk::Failure::FailureType::Off, motor_instance, |
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mavsdk::Failure::Result::Success); |
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std::this_thread::sleep_for(std::chrono::seconds(1)); |
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// Wait for RTL to trigger automatically
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std::chrono::seconds until_disarmed_timeout = std::chrono::seconds(180); |
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tester.wait_until_disarmed(until_disarmed_timeout); |
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tester.check_home_within(5.f); |
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} |
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TEST_CASE("Control Allocation - Terminate on motor failure", "[controlallocation]") |
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{ |
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const float flight_altitude = 100.0f; |
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const float hover_speed_tolerance = 1.0f; |
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AutopilotTesterFailure tester; |
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tester.connect(connection_url); |
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tester.wait_until_ready(); |
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|
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// Configuration
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tester.set_param_sys_failure_en(true); // Enable failure injection
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tester.set_param_fd_act_en(true); // Enable motor failure detection
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tester.set_param_mc_airmode(1); // Enable airmode for control allocation with motor failure
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tester.set_param_ca_failure_mode(1); // Enable control allocation handling of failed motor
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tester.set_param_com_act_fail_act(4); // Terminate on motor failure
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tester.set_takeoff_altitude(flight_altitude); |
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std::this_thread::sleep_for(std::chrono::seconds( |
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1)); // This is necessary for the takeoff altitude to be applied properly
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// Takeoff
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tester.arm(); |
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tester.takeoff(); |
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tester.wait_until_altitude(flight_altitude, std::chrono::seconds(60)); |
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tester.wait_until_speed_lower_than(hover_speed_tolerance, std::chrono::seconds(60)); |
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// Motor failure mid-air
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const int motor_instance = 1; |
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tester.inject_failure(mavsdk::Failure::FailureUnit::SystemMotor, mavsdk::Failure::FailureType::Off, motor_instance, |
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mavsdk::Failure::Result::Success); |
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std::this_thread::sleep_for(std::chrono::seconds(1)); |
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// Wait for disarm with a low enough timeout such that it's necessary for the
|
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// drone to freefall (terminate) in order to disarm quickly enough:
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// h = g/2 * t^2 -> solve for t
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const int seconds_to_touchdown = 2 + sqrt(flight_altitude * 2 / 10.0); |
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std::cout << "seconds_to_touchdown: " << seconds_to_touchdown << std::endl; |
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std::chrono::seconds until_disarmed_timeout = std::chrono::seconds(seconds_to_touchdown); |
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tester.wait_until_disarmed(until_disarmed_timeout); |
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} |
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#if 0 |
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// This is for checking that the SITL test is actually capable of detecting the drone crash
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// when not reallocating the control allocation on a motor failure
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TEST_CASE("Control Allocation - Remove two motors and expect crash", "[controlallocation]") |
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{ |
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// TODO
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} |
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#endif |
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#if 0 |
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TEST_CASE("Control Allocation with multiple sequential motor failures", "[controlallocation]") |
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{ |
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// TODO
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} |
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#endif |
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|
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#if 0 |
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TEST_CASE("Control Allocation with multiple simultaneous motor failures", "[controlallocation]") |
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{ |
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// TODO
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} |
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#endif |
@ -0,0 +1,61 @@
@@ -0,0 +1,61 @@
|
||||
/****************************************************************************
|
||||
* |
||||
* Copyright (c) 2021 PX4 Development Team. All rights reserved. |
||||
* |
||||
* Redistribution and use in source and binary forms, with or without |
||||
* modification, are permitted provided that the following conditions |
||||
* are met: |
||||
* |
||||
* 1. Redistributions of source code must retain the above copyright |
||||
* notice, this list of conditions and the following disclaimer. |
||||
* 2. Redistributions in binary form must reproduce the above copyright |
||||
* notice, this list of conditions and the following disclaimer in |
||||
* the documentation and/or other materials provided with the |
||||
* distribution. |
||||
* 3. Neither the name PX4 nor the names of its contributors may be |
||||
* used to endorse or promote products derived from this software |
||||
* without specific prior written permission. |
||||
* |
||||
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS |
||||
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT |
||||
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS |
||||
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE |
||||
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, |
||||
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, |
||||
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS |
||||
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED |
||||
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT |
||||
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN |
||||
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
||||
* POSSIBILITY OF SUCH DAMAGE. |
||||
* |
||||
****************************************************************************/ |
||||
|
||||
#include <thread> |
||||
#include <chrono> |
||||
|
||||
#include "autopilot_tester_failure.h" |
||||
|
||||
TEST_CASE("Failure Injection - Reject mid-air when it is disabled", "[multicopter]") |
||||
{ |
||||
AutopilotTesterFailure tester; |
||||
tester.connect(connection_url); |
||||
tester.wait_until_ready(); |
||||
tester.arm(); |
||||
tester.takeoff(); |
||||
tester.wait_until_hovering(); |
||||
tester.inject_failure(mavsdk::Failure::FailureUnit::SystemMotor, mavsdk::Failure::FailureType::Off, 1, |
||||
mavsdk::Failure::Result::Disabled); |
||||
tester.execute_rtl(); |
||||
std::chrono::seconds until_disarmed_timeout = std::chrono::seconds(180); |
||||
tester.wait_until_disarmed(until_disarmed_timeout); |
||||
} |
||||
|
||||
TEST_CASE("Failure Injection - Reject before arming", "[multicopter]") |
||||
{ |
||||
AutopilotTesterFailure tester; |
||||
tester.connect(connection_url); |
||||
tester.wait_until_ready(); |
||||
tester.inject_failure(mavsdk::Failure::FailureUnit::SystemMotor, mavsdk::Failure::FailureType::Off, 1, |
||||
mavsdk::Failure::Result::Disabled); |
||||
} |
Loading…
Reference in new issue