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https://github.com/ArduPilot/ardupilot
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Correct AP_TECS.cpp typos per magicrub comments
poper changed to proper
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@ -136,7 +136,7 @@ const AP_Param::GroupInfo AP_TECS::var_info[] = {
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// @Param: PITCH_MAX
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// @Param: PITCH_MAX
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// @DisplayName: Maximum pitch in auto flight
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// @DisplayName: Maximum pitch in auto flight
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// @Description: Overrides LIM_PITCH_MAX in automatic throttle modes to reduce climb rates. Uses LIM_PITCH_MAX if set to 0. For poper TECS tuning, set to the angle that the aircraft can climb at TRIM_ARSPD_CM and THR_MAX.
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// @Description: Overrides LIM_PITCH_MAX in automatic throttle modes to reduce climb rates. Uses LIM_PITCH_MAX if set to 0. For proper TECS tuning, set to the angle that the aircraft can climb at TRIM_ARSPD_CM and THR_MAX.
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// @Range: 0 45
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// @Range: 0 45
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// @Increment: 1
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// @Increment: 1
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// @User: Advanced
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// @User: Advanced
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@ -144,7 +144,7 @@ const AP_Param::GroupInfo AP_TECS::var_info[] = {
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// @Param: PITCH_MIN
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// @Param: PITCH_MIN
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// @DisplayName: Minimum pitch in auto flight
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// @DisplayName: Minimum pitch in auto flight
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// @Description: Overrides LIM_PITCH_MIN in automatic throttle modes to reduce descent rates. Uses LIM_PITCH_MIN if set to 0. For poper TECS tuning, set to the angle that the aircraft can descend at without overspeeding.
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// @Description: Overrides LIM_PITCH_MIN in automatic throttle modes to reduce descent rates. Uses LIM_PITCH_MIN if set to 0. For proper TECS tuning, set to the angle that the aircraft can descend at without overspeeding.
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// @Range: -45 0
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// @Range: -45 0
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// @Increment: 1
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// @Increment: 1
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// @User: Advanced
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// @User: Advanced
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@ -1104,4 +1104,4 @@ void AP_TECS::update_pitch_throttle(int32_t hgt_dem_cm,
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(double)logging.SPE_error,
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(double)logging.SPE_error,
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(double)logging.SEB_delta,
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(double)logging.SEB_delta,
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(double)load_factor);
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(double)load_factor);
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}
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}
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