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Roman BapstandThomas Stastny
dd2322d622
* created a Performance Model for fixed wing vehicle - added compensation for maximum climbrate, minimum sinkrate, minimum airspeed and trim airspeed based on weight ratio and air density - added atmosphere lib to standard atmosphere calculations --------- Signed-off-by: RomanBapst <bapstroman@gmail.com> Co-authored-by: Thomas Stastny <thomas.stastny@auterion.com>
66 lines
2.2 KiB
CMake
66 lines
2.2 KiB
CMake
############################################################################
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#
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# Copyright (c) 2015-2017 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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add_subdirectory(launchdetection)
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add_subdirectory(runway_takeoff)
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set(POSCONTROL_DEPENDENCIES
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launchdetection
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npfg
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runway_takeoff
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SlewRate
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tecs
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motion_planning
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performance_model
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)
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if(CONFIG_FIGURE_OF_EIGHT)
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add_subdirectory(figure_eight)
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set(POSCONTROL_DEPENDENCIES
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${POSCONTROL_DEPENDENCIES}
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figure_eight
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)
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endif()
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px4_add_module(
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MODULE modules__fw_pos_control
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MAIN fw_pos_control
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SRCS
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FixedwingPositionControl.cpp
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FixedwingPositionControl.hpp
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DEPENDS
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${POSCONTROL_DEPENDENCIES}
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)
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