forked from Archive/PX4-Autopilot
Added experimental LTO kconfig option
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@ -99,7 +99,7 @@
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#
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#=============================================================================
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cmake_minimum_required(VERSION 3.2 FATAL_ERROR)
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cmake_minimum_required(VERSION 3.9 FATAL_ERROR)
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set(PX4_SOURCE_DIR "${CMAKE_CURRENT_SOURCE_DIR}" CACHE FILEPATH "PX4 source directory" FORCE)
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set(PX4_BINARY_DIR "${CMAKE_CURRENT_BINARY_DIR}" CACHE FILEPATH "PX4 binary directory" FORCE)
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@ -234,6 +234,14 @@ message(STATUS "cmake build type: ${CMAKE_BUILD_TYPE}")
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#
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project(px4 CXX C ASM)
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# Check if LTO option and check if toolchain supports it
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if(LTO)
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include(CheckIPOSupported)
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check_ipo_supported()
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message(AUTHOR_WARNING "LTO enabled: LTO is highly experimental and should not be used in production")
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set(CMAKE_INTERPROCEDURAL_OPTIMIZATION TRUE)
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endif()
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set(package-contact "px4users@googlegroups.com")
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set(CMAKE_CXX_STANDARD 14)
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7
Kconfig
7
Kconfig
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@ -51,6 +51,13 @@ menu "Toolchain"
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string "Architecture"
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default ""
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config BOARD_LTO
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bool "(EXPERIMENTAL) Link Time Optimization (LTO)"
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default n
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help
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Enables LTO flag in linker
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Note: Highly EXPERIMENTAL, furthermore make sure you're using a modern compiler GCC 9 or later
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config BOARD_FULL_OPTIMIZATION
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bool "Full optmization (O3)"
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default n
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@ -88,7 +88,7 @@ public:
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private:
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void Run() override;
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Takeoff _takeoff; /**< state machine and ramp to bring the vehicle off the ground without jumps */
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TakeoffHandling _takeoff; /**< state machine and ramp to bring the vehicle off the ground without jumps */
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orb_advert_t _mavlink_log_pub{nullptr};
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@ -39,13 +39,13 @@
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#include <mathlib/mathlib.h>
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#include <lib/geo/geo.h>
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void Takeoff::generateInitialRampValue(float velocity_p_gain)
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void TakeoffHandling::generateInitialRampValue(float velocity_p_gain)
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{
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velocity_p_gain = math::max(velocity_p_gain, 0.01f);
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_takeoff_ramp_vz_init = -CONSTANTS_ONE_G / velocity_p_gain;
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}
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void Takeoff::updateTakeoffState(const bool armed, const bool landed, const bool want_takeoff,
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void TakeoffHandling::updateTakeoffState(const bool armed, const bool landed, const bool want_takeoff,
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const float takeoff_desired_vz, const bool skip_takeoff, const hrt_abstime &now_us)
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{
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_spoolup_time_hysteresis.set_state_and_update(armed, now_us);
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@ -109,7 +109,7 @@ void Takeoff::updateTakeoffState(const bool armed, const bool landed, const bool
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}
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}
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float Takeoff::updateRamp(const float dt, const float takeoff_desired_vz)
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float TakeoffHandling::updateRamp(const float dt, const float takeoff_desired_vz)
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{
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float upwards_velocity_limit = takeoff_desired_vz;
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@ -53,11 +53,11 @@ enum class TakeoffState {
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flight = takeoff_status_s::TAKEOFF_STATE_FLIGHT
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};
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class Takeoff
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class TakeoffHandling
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{
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public:
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Takeoff() = default;
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~Takeoff() = default;
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TakeoffHandling() = default;
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~TakeoffHandling() = default;
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// initialize parameters
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void setSpoolupTime(const float seconds) { _spoolup_time_hysteresis.set_hysteresis_time_from(false, seconds * 1_s); }
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@ -38,13 +38,13 @@
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TEST(TakeoffTest, Initialization)
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{
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Takeoff takeoff;
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TakeoffHandling takeoff;
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EXPECT_EQ(takeoff.getTakeoffState(), TakeoffState::disarmed);
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}
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TEST(TakeoffTest, RegularTakeoffRamp)
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{
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Takeoff takeoff;
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TakeoffHandling takeoff;
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takeoff.setSpoolupTime(1.f);
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takeoff.setTakeoffRampTime(2.0);
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takeoff.generateInitialRampValue(CONSTANTS_ONE_G / 0.5f);
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