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@ -233,7 +233,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
@@ -233,7 +233,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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bool reset_takeoff_sp = true; |
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bool reset_z_sp_dist = false; |
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float surface_offset = 0.0f; // Z of ground level
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float z_sp_dist = 0.0f; // distance to ground setpoint (positive)
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float sp_z_dist = 0.0f; // distance to ground setpoint (positive)
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float ref_alt = 0.0f; |
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hrt_abstime ref_timestamp = 0; |
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@ -346,6 +346,10 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
@@ -346,6 +346,10 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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float xy_sp_offs_max = params.xy_vel_max / params.xy_p * 2.0f; |
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float sp_move_rate[3] = { 0.0f, 0.0f, 0.0f }; |
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float sp_z = local_pos_sp.z; |
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float z = local_pos.z; |
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float vz = local_pos.vz; |
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if (control_mode.flag_control_manual_enabled) { |
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/* manual control */ |
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/* check for reference point updates and correct setpoint */ |
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@ -369,17 +373,23 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
@@ -369,17 +373,23 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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if (reset_z_sp_dist) { |
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reset_z_sp_dist = false; |
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surface_offset = local_pos.z + local_pos.dist_bottom; |
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z_sp_dist = -local_pos_sp.z + surface_offset; |
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sp_z_dist = -local_pos_sp.z + surface_offset; |
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mavlink_log_info(mavlink_fd, "[mpc] surface offset: %.2f", surface_offset); |
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} else { |
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if (local_pos.surface_bottom_timestamp != surface_bottom_timestamp) { |
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/* new surface level */ |
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z_sp_dist += local_pos.z + local_pos.dist_bottom - surface_offset; |
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sp_z_dist += local_pos.z + local_pos.dist_bottom - surface_offset; |
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} |
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surface_offset = local_pos.z + local_pos.dist_bottom; |
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} |
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z = -local_pos.dist_bottom; |
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vz = -local_pos.dist_bottom_rate; |
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/* move altitude setpoint according to ground distance */ |
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local_pos_sp.z = surface_offset - z_sp_dist; |
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local_pos_sp.z = surface_offset - sp_z_dist; |
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sp_z = -sp_z_dist; |
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} |
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/* move altitude setpoint with throttle stick */ |
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@ -388,7 +398,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
@@ -388,7 +398,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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if (z_sp_ctl != 0.0f) { |
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sp_move_rate[2] = -z_sp_ctl * params.z_vel_max; |
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local_pos_sp.z += sp_move_rate[2] * dt; |
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z_sp_dist -= sp_move_rate[2] * dt; // this will have effect only if distance sensor used
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sp_z_dist -= sp_move_rate[2] * dt; |
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// TODO add z_sp_dist correction here
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if (local_pos_sp.z > local_pos.z + z_sp_offs_max) { |
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@ -541,6 +551,8 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
@@ -541,6 +551,8 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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reset_man_sp_xy = true; |
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reset_man_sp_z = true; |
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sp_z = local_pos_sp.z; |
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} else { |
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/* no control (failsafe), loiter or stay on ground */ |
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if (local_pos.landed) { |
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@ -578,6 +590,8 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
@@ -578,6 +590,8 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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reset_auto_sp_xy = false; |
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} |
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sp_z = local_pos_sp.z; |
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} |
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/* publish local position setpoint */ |
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@ -585,7 +599,8 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
@@ -585,7 +599,8 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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/* run position & altitude controllers, calculate velocity setpoint */ |
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if (control_mode.flag_control_altitude_enabled) { |
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global_vel_sp.vz = pid_calculate(&z_pos_pid, local_pos_sp.z, local_pos.z, local_pos.vz - sp_move_rate[2], dt) + sp_move_rate[2]; |
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// TODO add feed-forward to PID library to allow limiting resulting value
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global_vel_sp.vz = pid_calculate(&z_pos_pid, sp_z, z, vz - sp_move_rate[2], dt) + sp_move_rate[2]; |
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} else { |
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reset_man_sp_z = true; |
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@ -639,7 +654,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
@@ -639,7 +654,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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mavlink_log_info(mavlink_fd, "[mpc] reset hovering thrust: %.2f", (double)i); |
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} |
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thrust_sp[2] = thrust_pid_calculate(&z_vel_pid, global_vel_sp.vz, local_pos.vz, dt, att.R[2][2]); |
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thrust_sp[2] = thrust_pid_calculate(&z_vel_pid, global_vel_sp.vz, vz, dt, att.R[2][2]); |
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att_sp.thrust = -thrust_sp[2]; |
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} else { |
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