Abstract
The maneuvering control logic that was developed to implement acrobatic maneuvers fully automatically on a miniature helicopter is described. The key component of this system is a state-machine maneuver execution logic that was inspired by an analysis of human pilot strategies. Conventional multivariable trim trajectory controllers were used before and on the exit from the maneuvers; bumpless transfer between these control modes was achieved through re-initialization of controller integrator states. Flight tests with this control logic demonstrated smooth maneuver entry, automatic recovery to a steady-state trim trajectory, and an ability to sequence maneuvers in a fully autonomous airshow-like sequence. This approach was flight tested with split-S, hammerhead, and 360-deg axial roll maneuvers, as well as a split-S-hamraerhead maneuver sequence. The maneuvering control logic can be used to automate a variety of other maneuvers.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 752-759 |
| Number of pages | 8 |
| Journal | Journal of Guidance, Control, and Dynamics |
| Volume | 27 |
| Issue number | 5 |
| DOIs | |
| State | Published - 2004 |
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