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unsave changes from prev commit

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This commit is contained in:
Marvin Harms
2022-06-29 14:01:47 +02:00
parent 717d61e094
commit 95a5081e64
2 changed files with 14 additions and 14 deletions
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src/modules/fw_dyn_soar_control/FixedwingPositionINDIControl.hpp
+4 -4
View File
@@ -166,7 +166,7 @@ private:
(ParamFloat<px4::params::DS_MASS>) _param_fw_mass,
(ParamFloat<px4::params::DS_WING_AREA>) _param_fw_wing_area,
(ParamFloat<px4::params::DS_RHO>) _param_rho,
// aerodynamic params
// aerodynamic params (INDI)
(ParamFloat<px4::params::DS_C_L0>) _param_fw_c_l0,
(ParamFloat<px4::params::DS_C_L1>) _param_fw_c_l1,
(ParamFloat<px4::params::DS_C_D0>) _param_fw_c_d0,
@@ -174,7 +174,7 @@ private:
(ParamFloat<px4::params::DS_C_D2>) _param_fw_c_d2,
(ParamFloat<px4::params::DS_AOA_OFFSET>) _param_aoa_offset,
(ParamFloat<px4::params::DS_STALL_SPEED>) _param_stall_speed,
// position INDI control params
// position PD control params
(ParamFloat<px4::params::DS_LIN_K_X>) _param_lin_k_x,
(ParamFloat<px4::params::DS_LIN_K_Y>) _param_lin_k_y,
(ParamFloat<px4::params::DS_LIN_K_Z>) _param_lin_k_z,
@@ -184,12 +184,12 @@ private:
(ParamFloat<px4::params::DS_LIN_FF_X>) _param_lin_ff_x,
(ParamFloat<px4::params::DS_LIN_FF_Y>) _param_lin_ff_y,
(ParamFloat<px4::params::DS_LIN_FF_Z>) _param_lin_ff_z,
// attitude INDI control params
// attitude PD control params
(ParamFloat<px4::params::DS_ROT_K_ROLL>) _param_rot_k_roll,
(ParamFloat<px4::params::DS_ROT_K_PITCH>) _param_rot_k_pitch,
(ParamFloat<px4::params::DS_ROT_C_ROLL>) _param_rot_c_roll,
(ParamFloat<px4::params::DS_ROT_C_PITCH>) _param_rot_c_pitch,
// low-level controller params
// low-level controller params (INDI)
(ParamFloat<px4::params::DS_K_ACT_ROLL>) _param_k_act_roll,
(ParamFloat<px4::params::DS_K_ACT_PITCH>) _param_k_act_pitch,
(ParamFloat<px4::params::DS_K_ACT_YAW>) _param_k_act_yaw,
src/modules/fw_dyn_soar_control/fw_dyn_soar_control_params.c
+10 -10
View File
@@ -201,8 +201,8 @@ PARAM_DEFINE_FLOAT(DS_STALL_SPEED, 9.0f);
* control gain of position PD-controller (body x-direction)
*
* @unit
* @min -10
* @max 10
* @min 0
* @max 100
* @decimal 1
* @increment 0.1
* @group FW DYN SOAR Control
@@ -213,8 +213,8 @@ PARAM_DEFINE_FLOAT(DS_LIN_K_X, 1.0f);
* control gain of position PD-controller (body y-direction)
*
* @unit
* @min -10
* @max 10
* @min 0
* @max 100
* @decimal 1
* @increment 0.1
* @group FW DYN SOAR Control
@@ -225,8 +225,8 @@ PARAM_DEFINE_FLOAT(DS_LIN_K_Y, 1.0f);
* control gain of position PD-controller (body z-direction)
*
* @unit
* @min -10
* @max 10
* @min 0
* @max 100
* @decimal 1
* @increment 0.1
* @group FW DYN SOAR Control
@@ -273,7 +273,7 @@ PARAM_DEFINE_FLOAT(DS_LIN_C_Z, 0.75f);
* acceleration feedback gain of position PD-controller (body x-direction)
*
* @unit
* @min -10
* @min 0
* @max 10
* @decimal 1
* @increment 0.1
@@ -285,7 +285,7 @@ PARAM_DEFINE_FLOAT(DS_LIN_FF_X, 0.5f);
* acceleration feedback gain of position PD-controller (body y-direction)
*
* @unit
* @min -10
* @min 0
* @max 10
* @decimal 1
* @increment 0.1
@@ -297,7 +297,7 @@ PARAM_DEFINE_FLOAT(DS_LIN_FF_Y, 0.5f);
* acceleration feedback gain of position PD-controller (body z-direction)
*
* @unit
* @min -10
* @min 0
* @max 10
* @decimal 1
* @increment 0.1
@@ -476,7 +476,7 @@ PARAM_DEFINE_FLOAT(DS_ORIGIN_ALT, 537.0f);
// ======================================================
/**
* integer in {0,1,2,3} defining the loiter trajectory
* integer in {0,1,2,3,4,5} defining the loiter trajectory
*
* @unit
* @min 0