NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Nonlinear Maneuver AutopilotTrajectory-control laws based on singular-perturbation theory and nonlinear dynamical modeling. Nonlinear maneuver autopilot commands flight-test trajectories of F-15 airplane. Underlying theory of controller enables separation of variables processed in fast and slow control loops, reducing amount of computation required.
Document ID
19920000151
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Menon, P. K. A. (Integrated Systems, Inc.)
Badgett, M. E. (Integrated Systems, Inc.)
Walker, R. A. (Integrated Systems, Inc.)
Date Acquired
August 15, 2013
Publication Date
March 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 3
ISSN: 0145-319X
Subject Category
Electronic Systems
Report/Patent Number
ARC-12560
ISSN: 0145-319X
Report Number: ARC-12560
Accession Number
92B10151
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitleN90-11487/TBSee AlsoNonlinear Maneuver Autopilot For The F-15 Aircraft"
No Preview Available