Nonlinear Controller Synthesis for Single-Input Multiple-Output Systems with Application to Cruise Missile-Reference-Cited by-同舟云学术

Nonlinear Controller Synthesis for Single-Input Multiple-Output Systems with Application to Cruise Missile

Published:2010-04 Issue:2 Volume:23 Page:105-110
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Nassirharand Amir¹

Affiliation:

1. Associate Professor, Dept. of Mechanical, Materials and Manufacturing Engineering, Faculty of Engineering, Univ. of Nottingham, Semenyih, Selangor 43500, Malaysia.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000012

Reference26 articles.

1. Large Angle-of-Attack Missile Control Concepts for Aerodynamically Controlled Missiles

2. Atherton D. P. Benouarets M. and Nanka B. O. (1993). “Design of nonlinear PID controllers for nonlinear plants.” Proc. IFAC World Congress IFAC Sydney Australia 355–358.

3. Compensation of Actuator Dynamics in Nonlinear Missile Control

4. Adaptive control for feedback-linearized missiles with uncertainties

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