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AP_TECS: convert remaining uses of TRIM_ARSPD_CM to AIRSPEED_CRUISE

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This commit is contained in:
Andrew Tridgell 2024-01-18 16:32:46 +11:00
parent 79ab474c51
commit c8813677b3
1 changed files with 3 additions and 3 deletions
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6
libraries/AP_TECS/AP_TECS.cpp
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@ -20,7 +20,7 @@ const AP_Param::GroupInfo AP_TECS::var_info[] = {
// @Param: CLMB_MAX // @Param: CLMB_MAX
// @DisplayName: Maximum Climb Rate (metres/sec) // @DisplayName: Maximum Climb Rate (metres/sec)
// @Description: Maximum demanded climb rate. Do not set higher than the climb speed at THR_MAX at TRIM_ARSPD_CM when the battery is at low voltage. Reduce value if airspeed cannot be maintained on ascent. Increase value if throttle does not increase significantly to ascend. // @Description: Maximum demanded climb rate. Do not set higher than the climb speed at THR_MAX at AIRSPEED_CRUISE when the battery is at low voltage. Reduce value if airspeed cannot be maintained on ascent. Increase value if throttle does not increase significantly to ascend.
// @Increment: 0.1 // @Increment: 0.1
// @Range: 0.1 20.0 // @Range: 0.1 20.0
// @User: Standard // @User: Standard
@ -28,7 +28,7 @@ const AP_Param::GroupInfo AP_TECS::var_info[] = {
// @Param: SINK_MIN // @Param: SINK_MIN
// @DisplayName: Minimum Sink Rate (metres/sec) // @DisplayName: Minimum Sink Rate (metres/sec)
// @Description: Minimum sink rate when at THR_MIN and TRIM_ARSPD_CM. // @Description: Minimum sink rate when at THR_MIN and AIRSPEED_CRUISE.
// @Increment: 0.1 // @Increment: 0.1
// @Range: 0.1 10.0 // @Range: 0.1 10.0
// @User: Standard // @User: Standard
@ -140,7 +140,7 @@ const AP_Param::GroupInfo AP_TECS::var_info[] = {
// @Param: PITCH_MAX // @Param: PITCH_MAX
// @DisplayName: Maximum pitch in auto flight // @DisplayName: Maximum pitch in auto flight
// @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. // @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 AIRSPEED_CRUISE and THR_MAX.
// @Range: 0 45 // @Range: 0 45
// @Increment: 1 // @Increment: 1
// @User: Advanced // @User: Advanced