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Renamed variable and added new setting nav_fw_pitch2thr_threshold
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9ef10703de
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5 changed files with 18 additions and 11 deletions
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@ -109,6 +109,7 @@ static const OSD_Entry cmsx_menuFixedWingEntries[] =
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OSD_SETTING_ENTRY("PITCH TO THR RATIO", SETTING_NAV_FW_PITCH2THR),
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OSD_SETTING_ENTRY("LOITER RADIUS", SETTING_NAV_FW_LOITER_RADIUS),
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OSD_SETTING_ENTRY("CONTROL SMOOTHNESS", SETTING_NAV_FW_CONTROL_SMOOTHNESS),
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OSD_SETTING_ENTRY("PITCH TO THR THRESHOLD", SETTING_NAV_FW_PITCH2THR_THRESHOLD),
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OSD_BACK_AND_END_ENTRY,
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};
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@ -2260,6 +2260,12 @@ groups:
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field: fw.pitch_to_throttle
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min: 0
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max: 100
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- name: nav_fw_pitch2thr_threshold
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description: "Threshold from zero pitch before pitch_to_throttle is applied [centidegrees]"
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default_value: "0"
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field: fw.pitch_to_throttle_thresh
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min: 0
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max: 100
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- name: nav_fw_loiter_radius
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description: "PosHold radius. 3000 to 7500 is a good value (30-75m) [cm]"
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default_value: "5000"
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@ -87,7 +87,7 @@ PG_REGISTER_ARRAY(navSafeHome_t, MAX_SAFE_HOMES, safeHomeConfig, PG_SAFE_HOME_CO
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PG_REGISTER_ARRAY(navWaypoint_t, NAV_MAX_WAYPOINTS, nonVolatileWaypointList, PG_WAYPOINT_MISSION_STORAGE, 0);
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#endif
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PG_REGISTER_WITH_RESET_TEMPLATE(navConfig_t, navConfig, PG_NAV_CONFIG, 7);
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PG_REGISTER_WITH_RESET_TEMPLATE(navConfig_t, navConfig, PG_NAV_CONFIG, 8);
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PG_RESET_TEMPLATE(navConfig_t, navConfig,
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.general = {
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@ -152,6 +152,7 @@ PG_RESET_TEMPLATE(navConfig_t, navConfig,
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.max_throttle = 1700,
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.min_throttle = 1200,
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.pitch_to_throttle = 10, // pwm units per degree of pitch (10pwm units ~ 1% throttle)
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.pitch_to_throttle_thresh = 0, // Threshold from zero pitch before pitch_to_throttle is applied [centidegrees]
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.loiter_radius = 5000, // 50m
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//Fixed wing landing
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@ -222,6 +222,7 @@ typedef struct navConfig_s {
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uint16_t min_throttle; // Minimum allowed throttle in auto mode
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uint16_t max_throttle; // Maximum allowed throttle in auto mode
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uint8_t pitch_to_throttle; // Pitch angle (in deg) to throttle gain (in 1/1000's of throttle) (*10)
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uint8_t pitch_to_throttle_thresh; // Threshold from zero pitch before pitch_to_throttle is applied [centidegrees]
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uint16_t loiter_radius; // Loiter radius when executing PH on a fixed wing
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int8_t land_dive_angle;
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uint16_t launch_velocity_thresh; // Velocity threshold for swing launch detection
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@ -463,18 +463,16 @@ int16_t applyFixedWingMinSpeedController(timeUs_t currentTimeUs)
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int16_t fixedWingPitchToThrottleCorrection(int16_t pitch)
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{
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const int16_t pitch_to_throttle_deadband = 30;
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if (pitch > pitch_to_throttle_deadband) {
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// Above positive pitch deadband
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return DECIDEGREES_TO_DEGREES(pitch - pitch_to_throttle_deadband) * navConfig()->fw.pitch_to_throttle;
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if (pitch > navConfig()->fw.pitch_to_throttle_thresh) {
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// Positive pitch above threshold
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return DECIDEGREES_TO_DEGREES(pitch - navConfig()->fw.pitch_to_throttle_thresh) * navConfig()->fw.pitch_to_throttle;
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}
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else if (pitch < -pitch_to_throttle_deadband) {
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// Below negative pitch deadband
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return DECIDEGREES_TO_DEGREES(pitch + pitch_to_throttle_deadband) * navConfig()->fw.pitch_to_throttle;
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else if (pitch < -navConfig()->fw.pitch_to_throttle_thresh) {
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// Negative pitch below threshold
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return DECIDEGREES_TO_DEGREES(pitch + navConfig()->fw.pitch_to_throttle_thresh) * navConfig()->fw.pitch_to_throttle;
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}
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else {
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// Inside deadband
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// Inside pitch_to_throttle_thresh deadband. Make no throttle correction.
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return 0;
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}
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}
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