SITL: remove zero initialisations, move more into class definitions
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@ -41,25 +41,7 @@ using namespace SITL;
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*/
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Aircraft::Aircraft(const char *frame_str) :
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ground_level(0.0f),
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frame_height(0.0f),
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dcm(),
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gyro(),
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velocity_ef(),
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mass(0.0f),
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accel_body(0.0f, 0.0f, -GRAVITY_MSS),
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time_now_us(0),
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gyro_noise(radians(0.1f)),
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accel_noise(0.3f),
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rate_hz(1200.0f),
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autotest_dir(nullptr),
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frame(frame_str),
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num_motors(1),
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#if defined(__CYGWIN__) || defined(__CYGWIN64__)
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min_sleep_time(20000)
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#else
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min_sleep_time(5000)
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#endif
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frame(frame_str)
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{
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// make the SIM_* variables available to simulator backends
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sitl = AP::sitl();
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@ -67,7 +49,6 @@ Aircraft::Aircraft(const char *frame_str) :
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set_speedup(1.0f);
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last_wall_time_us = get_wall_time_us();
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frame_counter = 0;
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// allow for orientation settings, such as with tailsitters
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enum ap_var_type ptype;
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@ -164,15 +164,15 @@ protected:
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Vector3f velocity_air_bf; // velocity relative to airmass, body frame
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Vector3f position; // meters, NED from origin
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float mass; // kg
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float external_payload_mass = 0.0f; // kg
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Vector3f accel_body; // m/s/s NED, body frame
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float external_payload_mass; // kg
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Vector3f accel_body{0.0f, 0.0f, -GRAVITY_MSS}; // m/s/s NED, body frame
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float airspeed; // m/s, apparent airspeed
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float airspeed_pitot; // m/s, apparent airspeed, as seen by fwd pitot tube
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float battery_voltage = -1.0f;
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float battery_current = 0.0f;
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float battery_current;
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uint8_t num_motors = 1;
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float rpm[12];
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uint8_t rcin_chan_count = 0;
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uint8_t rcin_chan_count;
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float rcin[12];
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float range = -1.0f; // externally supplied rangefinder value, assumed to have been corrected for vehicle attitude
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@ -192,17 +192,17 @@ protected:
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} wind_vane_apparent;
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// Wind Turbulence simulated Data
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float turbulence_azimuth = 0.0f;
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float turbulence_horizontal_speed = 0.0f; // m/s
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float turbulence_vertical_speed = 0.0f; // m/s
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float turbulence_azimuth;
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float turbulence_horizontal_speed; // m/s
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float turbulence_vertical_speed; // m/s
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Vector3f mag_bf; // local earth magnetic field vector in Gauss, earth frame
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uint64_t time_now_us;
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const float gyro_noise;
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const float accel_noise;
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float rate_hz;
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const float gyro_noise = radians(0.1f);
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const float accel_noise = 0.3f;
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float rate_hz = 1200.0f;
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float target_speedup;
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uint64_t frame_time_us;
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uint64_t last_wall_time_us;
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@ -289,10 +289,14 @@ protected:
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float get_local_updraft(Vector3f currentPos);
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private:
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uint64_t last_time_us = 0;
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uint32_t frame_counter = 0;
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uint64_t last_time_us;
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uint32_t frame_counter;
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uint32_t last_ground_contact_ms;
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const uint32_t min_sleep_time;
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#if defined(__CYGWIN__) || defined(__CYGWIN64__)
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const uint32_t min_sleep_time{20000};
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#else
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const uint32_t min_sleep_time{5000};
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#endif
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struct {
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Vector3f accel_body;
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@ -24,8 +24,7 @@
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using namespace SITL;
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MultiCopter::MultiCopter(const char *frame_str) :
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Aircraft(frame_str),
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frame(nullptr)
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Aircraft(frame_str)
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{
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mass = 1.5f;
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@ -24,13 +24,7 @@
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namespace SITL {
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SimRover::SimRover(const char *frame_str) :
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Aircraft(frame_str),
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max_speed(20),
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max_accel(10),
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max_wheel_turn(35),
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turning_circle(1.8),
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skid_turn_rate(140), // degrees/sec
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skid_steering(false)
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Aircraft(frame_str)
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{
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skid_steering = strstr(frame_str, "skid") != nullptr;
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@ -38,11 +38,11 @@ public:
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}
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private:
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float max_speed;
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float max_accel;
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float max_wheel_turn;
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float turning_circle;
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float skid_turn_rate;
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float max_speed = 20.0f;
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float max_accel = 10.0f;
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float max_wheel_turn = 35.0f;
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float turning_circle = 1.8f;
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float skid_turn_rate = 140.0f;
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bool skid_steering;
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float turn_circle(float steering);
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@ -22,11 +22,6 @@
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namespace SITL {
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Tracker::Tracker(const char *frame_str) :
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Aircraft(frame_str)
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{}
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/*
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update function for position (normal) servos.
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*/
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@ -27,7 +27,8 @@ namespace SITL {
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*/
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class Tracker : public Aircraft {
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public:
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Tracker(const char *frame_str);
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using Aircraft::Aircraft;
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void update(const struct sitl_input &input) override;
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/* static object creator */
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@ -44,7 +45,7 @@ private:
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const float yaw_range = 170;
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const float zero_yaw = 270; // yaw direction at startup
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const float zero_pitch = 10; // pitch at startup
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uint64_t last_debug_us = 0;
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uint64_t last_debug_us;
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float pitch_input;
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float yaw_input;
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