AP_MotorsHeli: swash and tail servo objects moved into class
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08a485eec4
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@ -115,7 +115,25 @@ const AP_Param::GroupInfo AP_MotorsHeli_Single::var_info[] = {
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// @Increment: 1
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// @User: Standard
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AP_GROUPINFO("GYR_GAIN_ACRO", 11, AP_MotorsHeli_Single, _ext_gyro_gain_acro, 0),
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// @Group: SV1_
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// @Path: ../RC_Channel/RC_Channel.cpp
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AP_SUBGROUPINFO(_swash_servo_1, "SV1_", 12, AP_MotorsHeli_Single, RC_Channel),
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// @Group: SV2_
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// @Path: ../RC_Channel/RC_Channel.cpp
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AP_SUBGROUPINFO(_swash_servo_2, "SV2_", 13, AP_MotorsHeli_Single, RC_Channel),
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// @Group: SV3_
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// @Path: ../RC_Channel/RC_Channel.cpp
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AP_SUBGROUPINFO(_swash_servo_3, "SV3_", 14, AP_MotorsHeli_Single, RC_Channel),
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// @Group: SV4_
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// @Path: ../RC_Channel/RC_Channel.cpp
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AP_SUBGROUPINFO(_yaw_servo, "SV4_", 15, AP_MotorsHeli_Single, RC_Channel),
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// parameters up to and including 29 are reserved for tradheli
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AP_GROUPEND
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};
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@ -45,21 +45,13 @@ class AP_MotorsHeli_Single : public AP_MotorsHeli {
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public:
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// constructor
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AP_MotorsHeli_Single(RC_Channel& servo_aux,
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RC_Channel& servo_rsc,
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RC_Channel& servo_1,
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RC_Channel& servo_2,
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RC_Channel& servo_3,
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RC_Channel& servo_4,
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uint16_t loop_rate,
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uint16_t speed_hz = AP_MOTORS_HELI_SPEED_DEFAULT) :
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AP_MotorsHeli(loop_rate, speed_hz),
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_servo_aux(servo_aux),
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_swash_servo_1(servo_1),
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_swash_servo_2(servo_2),
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_swash_servo_3(servo_3),
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_yaw_servo(servo_4),
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_main_rotor(RC_Channel_aux::k_heli_rsc, AP_MOTORS_HELI_SINGLE_RSC, loop_rate),
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_tail_rotor(RC_Channel_aux::k_heli_tail_rsc, AP_MOTORS_HELI_SINGLE_AUX, loop_rate)
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_tail_rotor(RC_Channel_aux::k_heli_tail_rsc, AP_MOTORS_HELI_SINGLE_AUX, loop_rate),
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_swash_servo_1(CH_1), _swash_servo_2(CH_2), _swash_servo_3(CH_3), _yaw_servo(CH_4)
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{
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AP_Param::setup_object_defaults(this, var_info);
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};
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@ -140,11 +132,6 @@ protected:
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// external objects we depend upon
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RC_Channel& _servo_aux; // output to ext gyro gain and tail direct drive esc (ch7)
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RC_Channel& _swash_servo_1; // swash plate servo #1
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RC_Channel& _swash_servo_2; // swash plate servo #2
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RC_Channel& _swash_servo_3; // swash plate servo #3
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RC_Channel& _yaw_servo; // tail servo
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AP_MotorsHeli_RSC _main_rotor; // main rotor
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AP_MotorsHeli_RSC _tail_rotor; // tail rotor
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@ -168,6 +155,10 @@ protected:
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AP_Float _collective_yaw_effect; // Feed-forward compensation to automatically add rudder input when collective pitch is increased. Can be positive or negative depending on mechanics.
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AP_Int8 _flybar_mode; // Flybar present or not. Affects attitude controller used during ACRO flight mode
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AP_Int16 _direct_drive_tailspeed; // Direct Drive VarPitch Tail ESC speed (0 ~ 1000)
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RC_Channel _swash_servo_1; // swash plate servo #1
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RC_Channel _swash_servo_2; // swash plate servo #2
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RC_Channel _swash_servo_3; // swash plate servo #3
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RC_Channel _yaw_servo; // tail servo
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bool _acro_tail = false;
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};
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