Abstract
Autonomous air vehicles have numerous applications, all of which require the vehicle to have stable and accurate control of its motion. In this paper, a hierarchical control system for small autonomous helicopters is described. The control system consists of four components: a navigation filter, an inner-loop hover control system, a waypoint guidance system, and a ground-based flight manager. All four elements of the control system have been verified with flight tests of the Draper Small Autonomous Air Vehicle.
Original language | English (US) |
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Pages (from-to) | 3629-3634 |
Number of pages | 6 |
Journal | Proceedings of the IEEE Conference on Decision and Control |
Volume | 4 |
State | Published - Dec 1 1998 |
Externally published | Yes |