NASA Technical Reports Server (NTRS) : Nonlinear pdf

NASA Technical Reports Server (NTRS) : Nonlinear

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Description of the Book:

A methodology is described for the development of flight test trajectory control laws based on singular perturbation methodology and nonlinear dynamic modeling. The control design methodology is applied to a detailed nonlinear six degree-of-freedom simulation of the F-15 and results for a level accelerations, pushover/pullup maneuver, zoom and pushover maneuver, excess thrust windup turn, constant thrust windup turn, and a constant dynamic pressure/constant load factor trajectory are presented

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 6/1/1989
• Year: 1989
• Book Topics/Themes: NASA Technical Reports Server (NTRS), AIRCRAFT MANEUVERS, AUTOMATIC PILOTS, CONTROL THEORY, EXPERT SYSTEMS, F-15 AIRCRAFT, TRAJECTORY OPTIMIZATION, AIRCRAFT CONTROL, CONTROL SYSTEMS DESIGN, FAULT TOLERANCE, FLIGHT SIMULATION, PERTURBATION THEORY, Menon, P. K. A., Badgett, M. E., Walker, R. A

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