Synthesis of a helicopter nonlinear flight controller using approximate model inversion-Reference-Cited by-同舟云学术

Synthesis of a helicopter nonlinear flight controller using approximate model inversion

Published:1993-08 Issue:3-4 Volume:18 Page:89-100
ISSN:0895-7177
Container-title:Mathematical and Computer Modelling
language:en
Short-container-title:Mathematical and Computer Modelling

Author:

Prasad J.V.R.,Lipp A.M.

Publisher

Elsevier BV

Subject

Computer Science Applications,Modeling and Simulation

Reference18 articles.

1. Practical robustness testing for helicopter flight control systems;Osder,1991

2. Decoupling of a class of nonlinear systems and its application to an aircraft control problem;Asseo;Journal of Aircraft,1973

3. Application of nonlinear system inverses to automatic flight control designs—System concepts and flight evaluations;Meyer;Theory and Application of Optimal Control in Aerospace Systems,1981

4. Application of nonlinear transformations to automatic flight control;Meyer;Automatica,1984

5. Nonlinear flight test trajectory controllers for aircraft;Menon;Journal of Guidance, Control and Dynamics,1987

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