2 changed files with 26 additions and 94 deletions
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uint8 TECS_MODE_NORMAL = 0 |
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uint8 TECS_MODE_UNDERSPEED = 1 |
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uint8 TECS_MODE_TAKEOFF = 2 |
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uint8 TECS_MODE_LAND = 3 |
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uint8 TECS_MODE_LAND_THROTTLELIM = 4 |
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uint8 TECS_MODE_BAD_DESCENT = 5 |
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uint8 TECS_MODE_CLIMBOUT = 6 |
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uint64 timestamp # timestamp, in microseconds since system start */ |
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float32 altitudeSp |
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float32 altitude_filtered |
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float32 flightPathAngleSp |
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float32 flightPathAngle |
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float32 flightPathAngleFiltered |
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float32 airspeedSp |
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float32 airspeed_filtered |
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float32 airspeedDerivativeSp |
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float32 airspeedDerivative |
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float32 totalEnergyRateSp |
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float32 totalEnergyRate |
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float32 energyDistributionRateSp |
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float32 energyDistributionRate |
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uint8 mode |
@ -1,94 +0,0 @@
@@ -1,94 +0,0 @@
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/****************************************************************************
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* |
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* Copyright (c) 2012-2014 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 |
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* modification, are permitted provided that the following conditions |
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* are met: |
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* |
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* 1. Redistributions of source code must retain the above copyright |
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* 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 |
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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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/**
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* @file vehicle_global_position.h |
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* Definition of the global fused WGS84 position uORB topic. |
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* |
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* @author Thomas Gubler <thomasgubler@student.ethz.ch> |
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*/ |
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#ifndef TECS_STATUS_T_H_ |
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#define TECS_STATUS_T_H_ |
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#include <stdint.h> |
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#include <stdbool.h> |
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#include "../uORB.h" |
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/**
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* @addtogroup topics |
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* @{ |
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*/ |
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typedef enum { |
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TECS_MODE_NORMAL = 0, |
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TECS_MODE_UNDERSPEED, |
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TECS_MODE_TAKEOFF, |
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TECS_MODE_LAND, |
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TECS_MODE_LAND_THROTTLELIM, |
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TECS_MODE_BAD_DESCENT, |
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TECS_MODE_CLIMBOUT |
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} tecs_mode; |
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/**
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* Internal values of the (m)TECS fixed wing speed alnd altitude control system |
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*/ |
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struct tecs_status_s { |
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uint64_t timestamp; /**< timestamp, in microseconds since system start */ |
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float altitudeSp; |
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float altitude_filtered; |
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float flightPathAngleSp; |
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float flightPathAngle; |
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float flightPathAngleFiltered; |
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float airspeedSp; |
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float airspeed_filtered; |
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float airspeedDerivativeSp; |
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float airspeedDerivative; |
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float totalEnergyRateSp; |
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float totalEnergyRate; |
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float energyDistributionRateSp; |
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float energyDistributionRate; |
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tecs_mode mode; |
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}; |
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/**
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* @} |
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*/ |
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/* register this as object request broker structure */ |
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ORB_DECLARE(tecs_status); |
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#endif |
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