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https://github.com/betaflight/betaflight.git
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hopefully the last cleanup of this test file
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parent
ee749af774
commit
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1 changed files with 9 additions and 16 deletions
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@ -15,7 +15,6 @@
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* along with Betaflight. If not, see <http://www.gnu.org/licenses/>.
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* along with Betaflight. If not, see <http://www.gnu.org/licenses/>.
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*/
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*/
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#include <stdint.h>
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#include <stdint.h>
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#include <stdbool.h>
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#include <stdbool.h>
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#include <limits.h>
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#include <limits.h>
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@ -46,7 +45,6 @@ extern "C" {
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#include "sensors/acceleration.h"
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#include "sensors/acceleration.h"
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#include "sensors/gyro.h"
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#include "sensors/gyro.h"
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PG_REGISTER(accelerometerConfig_t, accelerometerConfig, PG_ACCELEROMETER_CONFIG, 0);
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PG_REGISTER(accelerometerConfig_t, accelerometerConfig, PG_ACCELEROMETER_CONFIG, 0);
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PG_REGISTER(altHoldConfig_t, altHoldConfig, PG_ALTHOLD_CONFIG, 0);
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PG_REGISTER(altHoldConfig_t, altHoldConfig, PG_ALTHOLD_CONFIG, 0);
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PG_REGISTER(autopilotConfig_t, autopilotConfig, PG_AUTOPILOT, 0);
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PG_REGISTER(autopilotConfig_t, autopilotConfig, PG_AUTOPILOT, 0);
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@ -54,13 +52,9 @@ extern "C" {
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PG_REGISTER(positionConfig_t, positionConfig, PG_POSITION, 0);
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PG_REGISTER(positionConfig_t, positionConfig, PG_POSITION, 0);
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PG_REGISTER(rcControlsConfig_t, rcControlsConfig, PG_RC_CONTROLS_CONFIG, 0);
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PG_REGISTER(rcControlsConfig_t, rcControlsConfig, PG_RC_CONTROLS_CONFIG, 0);
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// void altHoldInit(void);
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// void updateAltHoldState(timeUs_t);
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bool failsafeIsActive(void) { return false; }
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bool failsafeIsActive(void) { return false; }
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timeUs_t currentTimeUs = 0;
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timeUs_t currentTimeUs = 0;
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bool isAltHoldActive();
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bool isAltHoldActive();
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gpsSolutionData_t gpsSol;
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}
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}
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#include "unittest_macros.h"
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#include "unittest_macros.h"
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@ -71,7 +65,6 @@ uint32_t millis() {
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return millisRW;
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return millisRW;
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}
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}
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TEST(AltholdUnittest, altHoldTransitionsTest)
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TEST(AltholdUnittest, altHoldTransitionsTest)
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{
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{
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updateAltHoldState(currentTimeUs);
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updateAltHoldState(currentTimeUs);
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@ -107,15 +100,22 @@ TEST(AltholdUnittest, altHoldTransitionsTestUnfinishedExitEnter)
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// STUBS
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// STUBS
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extern "C" {
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extern "C" {
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uint8_t armingFlags = 0;
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int16_t debug[DEBUG16_VALUE_COUNT];
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uint8_t debugMode;
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uint16_t flightModeFlags = 0;
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uint8_t stateFlags = 0;
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acc_t acc;
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acc_t acc;
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attitudeEulerAngles_t attitude;
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gpsSolutionData_t gpsSol;
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float getAltitudeCm(void) {return 0.0f;}
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float getAltitudeCm(void) {return 0.0f;}
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float getAltitudeDerivative(void) {return 0.0f;}
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float getAltitudeDerivative(void) {return 0.0f;}
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float getCosTiltAngle(void) { return 0.0f; }
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float getCosTiltAngle(void) { return 0.0f; }
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float rcCommand[4];
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attitudeEulerAngles_t attitude;
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float getGpsDataIntervalSeconds(void) { return 0.01f; }// gpsSolutionData_t gpsSol;
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float getGpsDataIntervalSeconds(void) { return 0.01f; }// gpsSolutionData_t gpsSol;
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bool isNewGPSDataAvailable(void){ return true; }
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bool isNewGPSDataAvailable(void){ return true; }
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float rcCommand[4];
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float vector2Norm(const vector2_t *v) {
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float vector2Norm(const vector2_t *v) {
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UNUSED(*v);
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UNUSED(*v);
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@ -184,11 +184,4 @@ void GPS_distances(const gpsLocation_t *from, const gpsLocation_t *to, float *pE
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UNUSED(input);
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UNUSED(input);
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return 0.0;
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return 0.0;
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}
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}
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int16_t debug[DEBUG16_VALUE_COUNT];
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uint8_t debugMode;
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uint8_t armingFlags = 0;
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uint8_t stateFlags = 0;
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uint16_t flightModeFlags = 0;
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}
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}
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