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Plane: remove unused params

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Iampete1 2021-09-04 17:08:24 +01:00 committed by Andrew Tridgell
parent 1057161f88
commit fd7a879c85
2 changed files with 3 additions and 21 deletions
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7
ArduPlane/Parameters.cpp
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@ -222,13 +222,6 @@ const AP_Param::Info Plane::var_info[] = {
// @User: Standard
GSCALAR(nav_controller, "NAV_CONTROLLER", AP_Navigation::CONTROLLER_L1),
// @Param: ALT_CTRL_ALG
// @DisplayName: Altitude control algorithm
// @Description: This sets what algorithm will be used for altitude control. The default is zero, which selects the most appropriate algorithm for your airframe. Currently the default is to use TECS (total energy control system). From time to time we will add other experimental altitude control algorithms which will be selected using this parameter.
// @Values: 0:Automatic
// @User: Advanced
GSCALAR(alt_control_algorithm, "ALT_CTRL_ALG", ALT_CONTROL_DEFAULT),
// @Param: ALT_OFFSET
// @DisplayName: Altitude offset
// @Description: This is added to the target altitude in automatic flight. It can be used to add a global altitude offset to a mission

17
ArduPlane/Parameters.h
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@ -83,7 +83,7 @@ public:
k_param_vtail_output, // unused
k_param_nav_controller,
k_param_elevon_output, // unused
k_param_att_controller,
k_param_att_controller, // unused
k_param_mixing_gain,
k_param_scheduler,
k_param_relay,
@ -173,7 +173,7 @@ public:
k_param_airspeed_max,
k_param_FBWB_min_altitude_cm, // 0=disabled, minimum value for altitude in cm (for first time try 30 meters = 3000 cm)
k_param_flybywire_elev_reverse,
k_param_alt_control_algorithm,
k_param_alt_control_algorithm, // unused
k_param_flybywire_climb_rate,
k_param_acro_roll_rate,
k_param_acro_pitch_rate,
@ -305,7 +305,7 @@ public:
//
// 220: Waypoint data
//
k_param_waypoint_mode = 220,
k_param_waypoint_mode = 220, // unused
k_param_command_total, // unused
k_param_command_index, // unused
k_param_waypoint_radius,
@ -380,18 +380,10 @@ public:
// navigation controller type. See AP_Navigation::ControllerType
AP_Int8 nav_controller;
// attitude controller type.
AP_Int8 att_controller;
AP_Int8 auto_fbw_steer;
// Estimation
//
AP_Int8 alt_control_algorithm;
// Waypoints
//
AP_Int8 waypoint_mode;
AP_Int16 waypoint_radius;
AP_Int16 waypoint_max_radius;
AP_Int16 rtl_radius;
@ -517,9 +509,6 @@ public:
// dual motor tailsitter rudder to differential thrust scaling: 0-100%
AP_Int8 rudd_dt_gain;
// QACRO mode max yaw rate in deg/sec
AP_Int16 acro_yaw_rate;
// mask of channels to do manual pass-thru for
AP_Int32 manual_rc_mask;