AIRCRAFT FLIGHT TEST TRAJECTORY CONTROL.

被引：0
|
作者：
Menon, P.K.A. [1 ]
Walker, R.A. [1 ]
机构：
[1] Integrated Systems Inc, Palo Alto,, CA, USA, Integrated Systems Inc, Palo Alto, CA, USA
来源：
NASA Contractor Reports | 1988年 / 4161期
关键词：
AIRCRAFT; MILITARY - CONTROL SYSTEMS;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
This report compares two control law design techniques and evaluates the performance of the resulting controllers. 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 report details the maneuver modeling, linearization, and design methodologies utilized in this research. The results of applying these FTTCs to a nonlinear F-15 simulation are presented.
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