Decentralized integrated control of hypersonic vehicles
Abstract
This paper describes a design methodology for integrated control of hypersonic vehicles. The methodology adopts a hierarchical structure for design of integrated engine airframe control with resulting simplicity in both design and implementation phases. Additionally, the developed control laws provide the means for a decentralized implementation. Developed controls are contrasted against a nonintegrated control for decreased stabilizing control power requirements.
- Publication:
-
AIAA, Aerospace Sciences Meeting
- Pub Date:
- October 1990
- Bibcode:
- 1990aiaa.meetRT...S
- Keywords:
-
- Control Systems Design;
- Engine Airframe Integration;
- Flight Control;
- Hypersonic Vehicles;
- Aircraft Control;
- Equations Of Motion;
- Flight Conditions;
- Perturbation Theory;
- Launch Vehicles and Space Vehicles