ekf2_main - Add optical flow innovation pre-flight check (#13036)

* ekf2: Add FirstOrderLpf and InnovationLpf classes for innovation lowpass filtering

* ekf2: use InnovLpf filter class in preflight checks

* ekf2: move selection of yaw test limit for pre-flight check in function

* ekf2: Move pre-flight checks into separate function

* ekf2: use static constexpr insetead of inline for sq (square) function

* ekf2: Split pre-flight checks in separate functions
Also use the same check for all the innovations:
innov_lpf < test and innov < 2xtest

* ekf2: Add optical flow pre-flight check

* ekf2: Combine FirstOrderLpf and InnovationLpf in single class

* ekf2: check vel_pos_innov when ev_pos is active as well

* ekf2: transform InnovationLpf into a header only library and pass the
spike limit during the update call to avoid storing it here

* ekf2: Static and const cleanup
- set spike_lim constants as static constexpr, set innovation
- set checker helper functions as static
- rename the mix of heading and yaw as heading to avoid confusion

* ekf2: use ternary operator in selectHeadingTestLimit instead of if-else

* ekf2: store intermediate redults in const bool flags. Those will be used for logging

* ekf2: set variable const whenever possible

* ekf2: create PreFlightChecker class that handle all the innovation
pre-flight checks.
Add simple unit testing
Use bitmask instead of general flag to have more granularity

* PreFlightChecker: use setter for the innovations to check instead of sending booleans in the update function
This makes it more scalable as more checks will be added

* ekf: Use booleans instead of bitmask for ekf preflt checks
Rename "down" to "vert"
This commit is contained in:
Mathieu Bresciani
2019-10-22 16:22:42 +02:00
committed by GitHub
parent 644c816a2a
commit 549fb0d5de
9 changed files with 620 additions and 87 deletions
+45
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############################################################################
#
# Copyright (c) 2019 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.
#
#############################################################################
px4_add_library(Ekf2Utility
PreFlightChecker.cpp
)
target_include_directories(Ekf2Utility
PUBLIC
${CMAKE_CURRENT_SOURCE_DIR}
)
target_link_libraries(Ekf2Utility PRIVATE mathlib)
px4_add_unit_gtest(SRC PreFlightCheckerTest.cpp LINKLIBS Ekf2Utility)
@@ -0,0 +1,79 @@
/****************************************************************************
*
* Copyright (c) 2019 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.
*
****************************************************************************/
/**
* First order "alpha" IIR digital filter with input saturation
*/
#include <mathlib/mathlib.h>
class InnovationLpf final
{
public:
InnovationLpf() = default;
~InnovationLpf() = default;
void reset(float val = 0.f) { _x = val; }
/**
* Update the filter with a new value and returns the filtered state
* The new value is constained by the limit set in setSpikeLimit
* @param val new input
* @param alpha normalized weight of the new input
* @param spike_limit the amplitude of the saturation at the input of the filter
* @return filtered output
*/
float update(float val, float alpha, float spike_limit)
{
float val_constrained = math::constrain(val, -spike_limit, spike_limit);
float beta = 1.f - alpha;
_x = beta * _x + alpha * val_constrained;
return _x;
}
/**
* Helper function to compute alpha from dt and the inverse of tau
* @param dt sampling time in seconds
* @param tau_inv inverse of the time constant of the filter
* @return alpha, the normalized weight of a new measurement
*/
static float computeAlphaFromDtAndTauInv(float dt, float tau_inv)
{
return dt * tau_inv;
}
private:
float _x; ///< current state of the filter
};
@@ -0,0 +1,142 @@
/****************************************************************************
*
* Copyright (c) 2019 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.
*
****************************************************************************/
/**
* @file PreFlightCheckHelper.cpp
* Class handling the EKF2 innovation pre flight checks
*/
#include "PreFlightChecker.hpp"
void PreFlightChecker::update(const float dt, const ekf2_innovations_s &innov)
{
const float alpha = InnovationLpf::computeAlphaFromDtAndTauInv(dt, _innov_lpf_tau_inv);
_has_heading_failed = preFlightCheckHeadingFailed(innov, alpha);
_has_horiz_vel_failed = preFlightCheckHorizVelFailed(innov, alpha);
_has_vert_vel_failed = preFlightCheckVertVelFailed(innov, alpha);
_has_height_failed = preFlightCheckHeightFailed(innov, alpha);
}
bool PreFlightChecker::preFlightCheckHeadingFailed(const ekf2_innovations_s &innov, const float alpha)
{
const float heading_test_limit = selectHeadingTestLimit();
const float heading_innov_spike_lim = 2.0f * heading_test_limit;
const float heading_innov_lpf = _filter_heading_innov.update(innov.heading_innov, alpha, heading_innov_spike_lim);
return checkInnovFailed(innov.heading_innov, heading_innov_lpf, heading_test_limit);
}
float PreFlightChecker::selectHeadingTestLimit()
{
// Select the max allowed heading innovaton depending on whether we are not aiding navigation using
// observations in the NE reference frame and if the vehicle can use GPS course to realign in flight (fixedwing sideslip fusion).
const bool is_ne_aiding = _is_using_gps_aiding || _is_using_ev_pos_aiding;
return (is_ne_aiding && !_can_observe_heading_in_flight)
? _nav_heading_innov_test_lim // more restrictive test limit
: _heading_innov_test_lim; // less restrictive test limit
}
bool PreFlightChecker::preFlightCheckHorizVelFailed(const ekf2_innovations_s &innov, const float alpha)
{
bool has_failed = false;
if (_is_using_gps_aiding || _is_using_ev_pos_aiding) {
const Vector2f vel_ne_innov = Vector2f(innov.vel_pos_innov);
Vector2f vel_ne_innov_lpf;
vel_ne_innov_lpf(0) = _filter_vel_n_innov.update(vel_ne_innov(0), alpha, _vel_innov_spike_lim);
vel_ne_innov_lpf(1) = _filter_vel_n_innov.update(vel_ne_innov(1), alpha, _vel_innov_spike_lim);
has_failed |= checkInnov2DFailed(vel_ne_innov, vel_ne_innov_lpf, _vel_innov_test_lim);
}
if (_is_using_flow_aiding) {
const Vector2f flow_innov = Vector2f(innov.flow_innov);
Vector2f flow_innov_lpf;
flow_innov_lpf(0) = _filter_flow_x_innov.update(flow_innov(0), alpha, _flow_innov_spike_lim);
flow_innov_lpf(1) = _filter_flow_x_innov.update(flow_innov(1), alpha, _flow_innov_spike_lim);
has_failed |= checkInnov2DFailed(flow_innov, flow_innov_lpf, _flow_innov_test_lim);
}
return has_failed;
}
bool PreFlightChecker::preFlightCheckVertVelFailed(const ekf2_innovations_s &innov, const float alpha)
{
const float vel_d_innov = innov.vel_pos_innov[2];
const float vel_d_innov_lpf = _filter_vel_d_innov.update(vel_d_innov, alpha, _vel_innov_spike_lim);
return checkInnovFailed(vel_d_innov, vel_d_innov_lpf, _vel_innov_test_lim);
}
bool PreFlightChecker::preFlightCheckHeightFailed(const ekf2_innovations_s &innov, const float alpha)
{
const float hgt_innov = innov.vel_pos_innov[5];
const float hgt_innov_lpf = _filter_hgt_innov.update(hgt_innov, alpha, _hgt_innov_spike_lim);
return checkInnovFailed(hgt_innov, hgt_innov_lpf, _hgt_innov_test_lim);
}
bool PreFlightChecker::checkInnovFailed(const float innov, const float innov_lpf, const float test_limit)
{
return fabsf(innov_lpf) > test_limit || fabsf(innov) > 2.0f * test_limit;
}
bool PreFlightChecker::checkInnov2DFailed(const Vector2f &innov, const Vector2f &innov_lpf, const float test_limit)
{
return innov_lpf.norm_squared() > sq(test_limit)
|| innov.norm_squared() > sq(2.0f * test_limit);
}
uint8_t PreFlightChecker::prefltFailBoolToBitMask(const bool heading_failed, const bool horiz_vel_failed,
const bool vert_vel_failed, const bool height_failed)
{
return heading_failed | (horiz_vel_failed << 1) | (vert_vel_failed << 2) | (height_failed << 3);
}
void PreFlightChecker::reset()
{
_is_using_gps_aiding = false;
_is_using_flow_aiding = false;
_is_using_ev_pos_aiding = false;
_has_heading_failed = false;
_has_horiz_vel_failed = false;
_has_vert_vel_failed = false;
_has_height_failed = false;
_filter_vel_n_innov.reset();
_filter_vel_e_innov.reset();
_filter_vel_d_innov.reset();
_filter_hgt_innov.reset();
_filter_heading_innov.reset();
_filter_flow_x_innov.reset();
_filter_flow_y_innov.reset();
}
@@ -0,0 +1,182 @@
/****************************************************************************
*
* Copyright (c) 2019 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.
*
****************************************************************************/
/**
* @file PreFlightChecker.hpp
* Class handling the EKF2 innovation pre flight checks
*
* First call the update(...) function and then get the results
* using the hasXxxFailed() getters
*/
#pragma once
#include <uORB/topics/vehicle_status.h>
#include <uORB/topics/ekf2_innovations.h>
#include <matrix/matrix/math.hpp>
#include "InnovationLpf.hpp"
using matrix::Vector2f;
class PreFlightChecker
{
public:
PreFlightChecker() = default;
~PreFlightChecker() = default;
/*
* Reset all the internal states of the class to their default value
*/
void reset();
/*
* Update the internal states
* @param dt the sampling time
* @param innov the ekf2_innovation_s struct containing the current innovations
*/
void update(float dt, const ekf2_innovations_s &innov);
/*
* If set to true, the checker will use a less conservative heading innovation check
*/
void setVehicleCanObserveHeadingInFlight(bool val) { _can_observe_heading_in_flight = val; }
void setUsingGpsAiding(bool val) { _is_using_gps_aiding = val; }
void setUsingFlowAiding(bool val) { _is_using_flow_aiding = val; }
void setUsingEvPosAiding(bool val) { _is_using_ev_pos_aiding = val; }
bool hasHeadingFailed() const { return _has_heading_failed; }
bool hasHorizVelFailed() const { return _has_horiz_vel_failed; }
bool hasVertVelFailed() const { return _has_vert_vel_failed; }
bool hasHeightFailed() const { return _has_height_failed; }
/*
* Overall state of the pre fligh checks
* @return true if any of the check failed
*/
bool hasFailed() const { return hasHorizFailed() || hasVertFailed(); }
/*
* Horizontal checks overall result
* @return true if one of the horizontal checks failed
*/
bool hasHorizFailed() const { return _has_heading_failed || _has_horiz_vel_failed; }
/*
* Vertical checks overall result
* @return true if one of the vertical checks failed
*/
bool hasVertFailed() const { return _has_vert_vel_failed || _has_height_failed; }
/*
* Check if the innovation fails the test
* To pass the test, the following conditions should be true:
* innov <= test_limit
* innov_lpf <= 2 * test_limit
* @param innov the current unfiltered innovation
* @param innov_lpf the low-pass filtered innovation
* @param test_limit the magnitude test limit
* @return true if the check failed the test, false otherwise
*/
static bool checkInnovFailed(float innov, float innov_lpf, float test_limit);
/*
* Check if the a innovation of a 2D vector fails the test
* To pass the test, the following conditions should be true:
* innov <= test_limit
* innov_lpf <= 2 * test_limit
* @param innov the current unfiltered innovation
* @param innov_lpf the low-pass filtered innovation
* @param test_limit the magnitude test limit
* @return true if the check failed the test, false otherwise
*/
static bool checkInnov2DFailed(const Vector2f &innov, const Vector2f &innov_lpf, float test_limit);
/*
* Packs the boolean flags into a bit field
*/
static uint8_t prefltFailBoolToBitMask(bool heading_failed, bool horiz_vel_failed, bool vert_vel_failed,
bool height_failed);
static constexpr float sq(float var) { return var * var; }
private:
bool preFlightCheckHeadingFailed(const ekf2_innovations_s &innov, float alpha);
float selectHeadingTestLimit();
bool preFlightCheckHorizVelFailed(const ekf2_innovations_s &innov, float alpha);
bool preFlightCheckVertVelFailed(const ekf2_innovations_s &innov, float alpha);
bool preFlightCheckHeightFailed(const ekf2_innovations_s &innov, float alpha);
void resetPreFlightChecks();
bool _has_heading_failed{};
bool _has_horiz_vel_failed{};
bool _has_vert_vel_failed{};
bool _has_height_failed{};
bool _can_observe_heading_in_flight{};
bool _is_using_gps_aiding{};
bool _is_using_flow_aiding{};
bool _is_using_ev_pos_aiding{};
// Low-pass filters for innovation pre-flight checks
InnovationLpf _filter_vel_n_innov; ///< Preflight low pass filter N axis velocity innovations (m/sec)
InnovationLpf _filter_vel_e_innov; ///< Preflight low pass filter E axis velocity innovations (m/sec)
InnovationLpf _filter_vel_d_innov; ///< Preflight low pass filter D axis velocity innovations (m/sec)
InnovationLpf _filter_hgt_innov; ///< Preflight low pass filter height innovation (m)
InnovationLpf _filter_heading_innov; ///< Preflight low pass filter heading innovation magntitude (rad)
InnovationLpf _filter_flow_x_innov; ///< Preflight low pass filter optical flow innovation (rad)
InnovationLpf _filter_flow_y_innov; ///< Preflight low pass filter optical flow innovation (rad)
// Preflight low pass filter time constant inverse (1/sec)
static constexpr float _innov_lpf_tau_inv = 0.2f;
// Maximum permissible velocity innovation to pass pre-flight checks (m/sec)
static constexpr float _vel_innov_test_lim = 0.5f;
// Maximum permissible height innovation to pass pre-flight checks (m)
static constexpr float _hgt_innov_test_lim = 1.5f;
// Maximum permissible yaw innovation to pass pre-flight checks when aiding inertial nav using NE frame observations (rad)
static constexpr float _nav_heading_innov_test_lim = 0.25f;
// Maximum permissible yaw innovation to pass pre-flight checks when not aiding inertial nav using NE frame observations (rad)
static constexpr float _heading_innov_test_lim = 0.52f;
// Maximum permissible flow innovation to pass pre-flight checks
static constexpr float _flow_innov_test_lim = 0.1f;
// Preflight velocity innovation spike limit (m/sec)
static constexpr float _vel_innov_spike_lim = 2.0f * _vel_innov_test_lim;
// Preflight position innovation spike limit (m)
static constexpr float _hgt_innov_spike_lim = 2.0f * _hgt_innov_test_lim;
// Preflight flow innovation spike limit (rad)
static constexpr float _flow_innov_spike_lim = 2.0f * _flow_innov_test_lim;
};
@@ -0,0 +1,108 @@
/****************************************************************************
*
* Copyright (C) 2019 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.
*
****************************************************************************/
/**
* Test code for PreFlightChecker class
* Run this test only using make tests TESTFILTER=PreFlightChecker
*/
#include <gtest/gtest.h>
#include "PreFlightChecker.hpp"
class PreFlightCheckerTest : public ::testing::Test
{
};
TEST_F(PreFlightCheckerTest, testInnovFailed)
{
const float test_limit = 1.0; ///< is the limit for innovation_lpf, the limit for innovation is 2*test_limit
const float innovations[9] = {0.0, 1.5, 2.5, -1.5, -2.5, 1.5, -1.5, -2.5, -2.5};
const float innovations_lpf[9] = {0.0, 0.9, 0.9, -0.9, -0.9, 1.1, -1.1, -1.1, 1.1};
const bool expected_result[9] = {false, false, true, false, true, true, true, true, true};
for (int i = 0; i < 9; i++) {
EXPECT_EQ(PreFlightChecker::checkInnovFailed(innovations[i], innovations_lpf[i], test_limit), expected_result[i]);
}
// Smaller test limit, all the checks should fail except the first
EXPECT_FALSE(PreFlightChecker::checkInnovFailed(innovations[0], innovations_lpf[0], 0.0));
for (int i = 1; i < 9; i++) {
EXPECT_TRUE(PreFlightChecker::checkInnovFailed(innovations[i], innovations_lpf[i], 0.0));
}
// Larger test limit, none of the checks should fail
for (int i = 0; i < 9; i++) {
EXPECT_FALSE(PreFlightChecker::checkInnovFailed(innovations[i], innovations_lpf[i], 2.0));
}
}
TEST_F(PreFlightCheckerTest, testInnov2dFailed)
{
const float test_limit = 1.0;
Vector2f innovations[4] = {{0.0, 0.0}, {0.0, 0.0}, {0.0, -2.5}, {1.5, -1.5}};
Vector2f innovations_lpf[4] = {{0.0, 0.0}, {1.1, 0.0}, {0.5, 0.5}, {1.0, -1.0}};
const bool expected_result[4] = {false, true, true, true};
for (int i = 0; i < 4; i++) {
EXPECT_EQ(PreFlightChecker::checkInnov2DFailed(innovations[i], innovations_lpf[i], test_limit), expected_result[i]);
}
// Smaller test limit, all the checks should fail except the first
EXPECT_FALSE(PreFlightChecker::checkInnov2DFailed(innovations[0], innovations_lpf[0], 0.0));
for (int i = 1; i < 4; i++) {
EXPECT_TRUE(PreFlightChecker::checkInnov2DFailed(innovations[i], innovations_lpf[i], 0.0));
}
// Larger test limit, none of the checks should fail
for (int i = 0; i < 4; i++) {
EXPECT_FALSE(PreFlightChecker::checkInnov2DFailed(innovations[i], innovations_lpf[i], 1.42));
}
}
TEST_F(PreFlightCheckerTest, testBitMask)
{
PreFlightChecker preflt_checker;
const bool heading_failed = true;
const bool horiz_vel_failed = true;
const bool down_vel_failed = false;
const bool height_failed = true;
int bitmask = PreFlightChecker::prefltFailBoolToBitMask(heading_failed, horiz_vel_failed, down_vel_failed,
height_failed);
EXPECT_EQ(bitmask, 0b1011);
}