A simple outer navigation loop is retained for navigation control. This will be replaced later. The pitch set point is hard coded to zero. Pitch stabilization should work.
This commit compiles, but needs further testing.
Arbitrary large limit values were hard coded into multirotor_attitude_control.c. These should be changed to parametric values or something sensible.
This commit will temporarily break fixedwing_control.c. A following commit will repair it along with significant changes to the inner loop control.
This commit has been tested to compile with fixedwing_control.c temporarily removed. No other testing has been completed.
Doug Weibel