Aircraft flight test trajectory control
- Author:
- Walker, R. A.
- Published:
- Sep 1, 1988.
- Physical Description:
- 1 electronic document
- Additional Creators:
- Menon, P. K. A.
- Access Online:
- hdl.handle.net
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- Summary:
- Two control law design techniques are compared and the performance of the resulting controllers evaluated. The design requirement is for a flight test trajectory controller (FTTC) capable of closed-loop, outer-loop control of an F-15 aircraft performing high-quality research flight test maneuvers. The maneuver modeling, linearization, and design methodologies utilized in this research, are detailed. The results of applying these FTTCs to a nonlinear F-15 simulation are presented.
- Collection:
- NASA Technical Reports Server (NTRS) Collection.
- Note:
- Document ID: 19890018045., Accession ID: 89N27416., NASA-CR-4161., NAS 1.26:4161., and H-1497.
- Terms of Use and Reproduction:
- No Copyright.
- Access Online:
- hdl.handle.net
View MARC record | catkey: 15689422