6 Commits

Include renames

Author	SHA1	Message	Date
mahima-yoga	8b3ef1cf9e	feat(navigator): add Guided Course mode for fixed-wing ... Implements a new GUIDED_COURSE navigator mode that maintains a constant ground-track bearing, altitude, and airspeed without manual stick input. The mode is activated via MAVLink and accepts real-time in-flight updates: - MAV_CMD_GUIDED_CHANGE_HEADING (HEADING_TYPE_COURSE_OVER_GROUND): set course - MAV_CMD_DO_CHANGE_ALTITUDE: adjust target altitude - MAV_CMD_DO_CHANGE_SPEED: adjust target airspeed On activation the vehicle captures its current velocity vector as the initial course bearing. A valid horizontal velocity estimate (GPS or dead-reckoning) is required; course commands are rejected if unavailable.	2026-05-27 10:51:55 +02:00
Silvan Fuhrer	82569aad8d	PositionSetpoint.msg: define range of loiter_radius ... Signed-off-by: Silvan Fuhrer <silvan@auterion.com>	2025-07-28 10:57:56 +02:00
Roman BapstandAlvaro Fernandez	c94c1ce4d2	Navigator: Support straight line mission landings (#23576) ... * introduced altitude acceptance radius in position setpoint for fixed wing guidance - allows navigator to explicitly set the altitude acceptance radius - needed for staright line landing support * added ignore_alt_acceptance to position setpoint message to allow guidance logic to ignore altitude error on waypoint - can be useful to prevent loitering at a waypoint within a mission landing sequence * only set altitude acceptance radius to infinity for a waypoint inside a mission landing for fixed wing vehicles * navigator: return altitude acceptance radius from triplet if it's valid * FixedWingPositionControl: check if alt acceptance radius provided in position setpoint is larger 0 --------- Signed-off-by: RomanBapst <bapstroman@gmail.com> Co-authored-by: Alvaro Fernandez <alvaro@auterion.com>	2024-09-10 17:44:24 +02:00
Silvan FuhrerandMatthias Grob	7e22b47b85	Navigator/FlightTaskAuto yaw handling improvements/simplifications (#22532) ... * PositionSetpoint: remove yaw_valid field * Navigator: set yaw setpoint to NAN for Takeoff Don't set a yaw setpoint for takeoff, as Navigator doesn't handle the yaw reset. The yaw setpoint generation is handled by FlightTaskAuto. * PositionSetpoint.msg: remove disable_weather_vane and instead only use the yaw field Strictly follow the concept that if the position_setpoint.yaw is set, then follow it the controller, and otherwise let the controller set it as it thinks it's best. * Navigator: remove logic that sets yaw to be accepted in TAKEOFF No longer needed as during Takeoff we anyway don't set a yaw setpoint. * PositionSetpoint.msg: remove yawspeed_valid * PositionSetpoint.msg: remove yawspeed * Navigator: set yaw setpoint to NAN instead of current In set_takeoff and set_land_item, as well as for VTOL transition. The flight tasks then set the yaw corresponding to the current yaw. * Navigator: change get_yaw_acceptance into a bool * PositionSetpoint.msg: improve comment for yaw * MissionBlock: remove unnecessary code from set_vtol_transition_item * Navigator: clean up calculate_breaking_stop(), set yaw to NAN * Navigator: set yaw to NAN in variouls places where not specifc setpoint is desired * Navigator: set yaw to NAN in reset_position_setpoint() --------- Signed-off-by: Silvan Fuhrer <silvan@auterion.com> Co-authored-by: Matthias Grob <maetugr@gmail.com>	2023-12-21 16:50:13 +01:00
Konrad	e5e66370e7	FixedwingPositionControl: Add support for figure 8 loitering. ... The command is sent by a dedicated mavlink command and forwarded to the fixed wing position controller. The pattern is defined by the radius of the major axis, the radius of the minor axis and the orientation. The pattern is then defined by: The upper part of the pattern consist of a clockwise circle with radius defined by the minor axis. The center of the circle is defined by the major axis minus the minor axis away from the pattern center. The lower part of the pattern consist of a counter-clockwise circle with the same definitions as above. In between, the circles are connected with straight lines in a cross configuration. The lines are always tangetial to the circles. The orientation rotates the major axis around the NED down axis. The loitering logic is defined inside its own class used by the fixed wing position control module. It defines which segment (one of the circles or lines) is active and uses the path controller (npfg or l1-control) to determine the desired roll angle. A feedback mavlink message is send with the executed pattern parameters.	2023-10-31 15:57:59 -04:00
Daniel Agar	cea185268e	msg ROS2 compatibility, microdds_client improvements (timesync, reduced code size, added topics, etc), fastrtps purge ... - update all msgs to be directly compatible with ROS2 - microdds_client improvements - timesync - reduced code size - add to most default builds if we can afford it - lots of other little changes - purge fastrtps (I tried to save this multiple times, but kept hitting roadblocks)	2022-10-19 19:36:47 -04:00