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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-21 07:23:34 +08:00
Rebase of changes to sensor_hil_fixedwing branch.
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@@ -108,7 +108,7 @@ int control_demo_main(int argc, char *argv[])
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deamon_task = task_spawn("control_demo",
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SCHED_DEFAULT,
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SCHED_PRIORITY_MAX - 10,
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4096,
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5120,
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control_demo_thread_main,
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(argv) ? (const char **)&argv[2] : (const char **)NULL);
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exit(0);
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@@ -6,31 +6,31 @@
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// 16 is max name length
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// gyro low pass filter
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PARAM_DEFINE_FLOAT(FWB_P_LP, 10.0f); // roll rate low pass cut freq
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PARAM_DEFINE_FLOAT(FWB_Q_LP, 10.0f); // pitch rate low pass cut freq
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PARAM_DEFINE_FLOAT(FWB_R_LP, 10.0f); // yaw rate low pass cut freq
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PARAM_DEFINE_FLOAT(FWB_P_LP, 300.0f); // roll rate low pass cut freq
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PARAM_DEFINE_FLOAT(FWB_Q_LP, 300.0f); // pitch rate low pass cut freq
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PARAM_DEFINE_FLOAT(FWB_R_LP, 300.0f); // yaw rate low pass cut freq
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// yaw washout
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PARAM_DEFINE_FLOAT(FWB_R_HP, 1.0f); // yaw rate high pass
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// stabilization mode
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PARAM_DEFINE_FLOAT(FWB_P2AIL, 0.1f); // roll rate 2 aileron
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PARAM_DEFINE_FLOAT(FWB_Q2ELV, 0.1f); // pitch rate 2 elevator
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PARAM_DEFINE_FLOAT(FWB_R2RDR, 0.1f); // yaw rate 2 rudder
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PARAM_DEFINE_FLOAT(FWB_P2AIL, 0.5f); // roll rate 2 aileron
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PARAM_DEFINE_FLOAT(FWB_Q2ELV, 0.5f); // pitch rate 2 elevator
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PARAM_DEFINE_FLOAT(FWB_R2RDR, 0.2f); // yaw rate 2 rudder
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// psi -> phi -> p
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PARAM_DEFINE_FLOAT(FWB_PSI2PHI, 2.0f); // heading 2 roll
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PARAM_DEFINE_FLOAT(FWB_PHI2P, 2.0f); // roll to roll rate
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PARAM_DEFINE_FLOAT(FWB_PHI_LIM_MAX, 1.0f); // roll limit
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PARAM_DEFINE_FLOAT(FWB_PSI2PHI, 0.5f); // heading 2 roll
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PARAM_DEFINE_FLOAT(FWB_PHI2P, 1.0f); // roll to roll rate
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PARAM_DEFINE_FLOAT(FWB_PHI_LIM_MAX, 0.5f); // roll limit, 28 deg
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// velocity -> theta
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PARAM_DEFINE_FLOAT(FWB_V2THE_P, 0.5f);
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PARAM_DEFINE_FLOAT(FWB_V2THE_P, 0.2f);
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PARAM_DEFINE_FLOAT(FWB_V2THE_I, 0.0f);
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PARAM_DEFINE_FLOAT(FWB_V2THE_D, 0.0f);
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PARAM_DEFINE_FLOAT(FWB_V2THE_D_LP, 0.0f);
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PARAM_DEFINE_FLOAT(FWB_V2THE_I_MAX, 0.0f);
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PARAM_DEFINE_FLOAT(FWB_THE_MIN, -1.0f);
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PARAM_DEFINE_FLOAT(FWB_THE_MAX, 1.0f);
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PARAM_DEFINE_FLOAT(FWB_THE_MIN, -0.5f);
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PARAM_DEFINE_FLOAT(FWB_THE_MAX, 0.5f);
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// theta -> q
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@@ -41,15 +41,15 @@ PARAM_DEFINE_FLOAT(FWB_THE2Q_D_LP, 0.0f);
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PARAM_DEFINE_FLOAT(FWB_THE2Q_I_MAX, 0.0f);
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// h -> thr
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PARAM_DEFINE_FLOAT(FWB_H2THR_P, 0.005f);
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PARAM_DEFINE_FLOAT(FWB_H2THR_I, 0.001f);
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PARAM_DEFINE_FLOAT(FWB_H2THR_D, 0.01f);
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PARAM_DEFINE_FLOAT(FWB_H2THR_D_LP, 1.0f);
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PARAM_DEFINE_FLOAT(FWB_H2THR_I_MAX, 250.0f);
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PARAM_DEFINE_FLOAT(FWB_H2THR_P, 0.01f);
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PARAM_DEFINE_FLOAT(FWB_H2THR_I, 0.0f);
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PARAM_DEFINE_FLOAT(FWB_H2THR_D, 0.0f);
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PARAM_DEFINE_FLOAT(FWB_H2THR_D_LP, 0.0f);
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PARAM_DEFINE_FLOAT(FWB_H2THR_I_MAX, 0.0f);
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// crosstrack
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PARAM_DEFINE_FLOAT(FWB_XT2YAW_MAX, 1.0f);
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PARAM_DEFINE_FLOAT(FWB_XT2YAW, 0.01f);
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PARAM_DEFINE_FLOAT(FWB_XT2YAW_MAX, 1.57f); // 90 deg
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PARAM_DEFINE_FLOAT(FWB_XT2YAW, 0.002f);
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// speed command
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PARAM_DEFINE_FLOAT(FWB_V_MIN, 20.0f);
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@@ -58,6 +58,6 @@ PARAM_DEFINE_FLOAT(FWB_V_MAX, 24.0f);
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// trim
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PARAM_DEFINE_FLOAT(FWB_TRIM_AIL, 0.0f);
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PARAM_DEFINE_FLOAT(FWB_TRIM_ELV, 0.0f);
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PARAM_DEFINE_FLOAT(FWB_TRIM_ELV, 0.005f);
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PARAM_DEFINE_FLOAT(FWB_TRIM_RDR, 0.0f);
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PARAM_DEFINE_FLOAT(FWB_TRIM_THR, 0.7f);
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PARAM_DEFINE_FLOAT(FWB_TRIM_THR, 0.81f);
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