Robust tracking control of an aircraft with critical actuator jam failures
Abstract
In this paper, we present a new single fixed controller approach based on the multivariable H2 control/regulator theory with internal model principle to solve a challenging control problem arising from an on‐flight critical elevator jam at random positions that otherwise would need switching numerous controllers or online adaptive redesign approaches.
Document Details
- Document Type
- Pub Defense Publication
- Publication Date
- Dec 25, 2019
- Source ID
- 10.1002/asjc.2280
Entities
People
- Bor‐Chin Chang
- Christine M. Belcastro
- Harry Kwatny
- Mevlut Bayram
- Po‐Chun Chan
Organizations
- Drexel University
- National Defense University
- United States Army Research Laboratory