Doug Weibel 4fea0a3fc1 This commit changes the inner loop control structures for fixed wing attitude control. Nested rate and angle loops are used with limits on both the rate setpoint ...

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.

2012-10-07 14:50:07 -06:00

..

fixedwing_control.c

This commit changes the inner loop control structures for fixed wing attitude control. Nested rate and angle loops are used with limits on both the rate setpoint

2012-10-07 14:50:07 -06:00

Makefile

Faster sensor bus resets on timeouts, massively reworked fixed wing app, tested

2012-08-05 15:56:24 +02:00