Daniel Agar
8 years ago
committed by
Lorenz Meier
15 changed files with 184 additions and 156 deletions
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#include "BlockSegwayController.hpp" |
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using matrix::Eulerf; |
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using matrix::Quatf; |
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void BlockSegwayController::update() |
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{ |
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// wait for a sensor update, check for exit condition every 100 ms
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if (px4_poll(&_attPoll, 1, 100) < 0) { return; } // poll error
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uint64_t newTimeStamp = hrt_absolute_time(); |
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float dt = (newTimeStamp - _timeStamp) / 1.0e6f; |
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_timeStamp = newTimeStamp; |
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// check for sane values of dt
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// to prevent large control responses
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if (dt > 1.0f || dt < 0) { return; } |
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// set dt for all child blocks
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setDt(dt); |
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// check for new updates
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if (_param_update.updated()) { updateParams(); } |
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// get new information from subscriptions
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updateSubscriptions(); |
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actuator_controls_s &actuators = _actuators.get(); |
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// default all output to zero unless handled by mode
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for (unsigned i = 2; i < actuator_controls_s::NUM_ACTUATOR_CONTROLS; i++) { |
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actuators.control[i] = 0.0f; |
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} |
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const uint8_t &nav_state = _status.get().nav_state; |
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// only update guidance in auto mode
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if (nav_state == vehicle_status_s::NAVIGATION_STATE_AUTO_MISSION) { |
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// update guidance
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} |
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Eulerf euler = Eulerf(Quatf(_att.get().q)); |
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// compute speed command
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float spdCmd = -th2v.update(euler.theta()) - q2v.update(_att.get().pitchspeed); |
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// handle autopilot modes
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if (nav_state == vehicle_status_s::NAVIGATION_STATE_AUTO_MISSION || |
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nav_state == vehicle_status_s::NAVIGATION_STATE_ALTCTL || |
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nav_state == vehicle_status_s::NAVIGATION_STATE_POSCTL) { |
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actuators.control[0] = spdCmd; |
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actuators.control[1] = spdCmd; |
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} else if (nav_state == vehicle_status_s::NAVIGATION_STATE_STAB) { |
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actuators.control[0] = spdCmd; |
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actuators.control[1] = spdCmd; |
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} else if (nav_state == vehicle_status_s::NAVIGATION_STATE_MANUAL) { |
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actuators.control[CH_LEFT] = _manual.get().z; |
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actuators.control[CH_RIGHT] = -_manual.get().x; |
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} |
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// update all publications
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updatePublications(); |
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} |
@ -1,60 +0,0 @@
@@ -1,60 +0,0 @@
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#include "BlockSegwayController.hpp" |
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void BlockSegwayController::update() |
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{ |
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// wait for a sensor update, check for exit condition every 100 ms
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if (px4_poll(&_attPoll, 1, 100) < 0) { return; } // poll error
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uint64_t newTimeStamp = hrt_absolute_time(); |
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float dt = (newTimeStamp - _timeStamp) / 1.0e6f; |
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_timeStamp = newTimeStamp; |
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// check for sane values of dt
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// to prevent large control responses
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if (dt > 1.0f || dt < 0) { return; } |
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// set dt for all child blocks
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setDt(dt); |
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// check for new updates
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if (_param_update.updated()) { updateParams(); } |
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// get new information from subscriptions
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updateSubscriptions(); |
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// default all output to zero unless handled by mode
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for (unsigned i = 2; i < NUM_ACTUATOR_CONTROLS; i++) { |
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_actuators.control[i] = 0.0f; |
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} |
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// only update guidance in auto mode
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if (_status.main_state == MAIN_STATE_AUTO) { |
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// update guidance
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} |
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// compute speed command
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float spdCmd = -th2v.update(_att.pitch) - q2v.update(_att.pitchspeed); |
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// handle autopilot modes
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if (_status.main_state == MAIN_STATE_AUTO || |
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_status.main_state == MAIN_STATE_ALTCTL || |
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_status.main_state == MAIN_STATE_POSCTL) { |
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_actuators.control[0] = spdCmd; |
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_actuators.control[1] = spdCmd; |
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} else if (_status.main_state == MAIN_STATE_MANUAL) { |
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if (_status.navigation_state == NAVIGATION_STATE_DIRECT) { |
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_actuators.control[CH_LEFT] = _manual.throttle; |
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_actuators.control[CH_RIGHT] = _manual.pitch; |
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} else if (_status.navigation_state == NAVIGATION_STATE_STABILIZE) { |
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_actuators.control[0] = spdCmd; |
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_actuators.control[1] = spdCmd; |
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} |
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} |
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// update all publications
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updatePublications(); |
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} |
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