Modern control theory for design of autopilots for bank-to-turn missiles-Reference-Cited by-同舟云学术

Modern control theory for design of autopilots for bank-to-turn missiles

Published:1987-07 Issue:4 Volume:10 Page:378-386
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Williams Douglas E.¹,Friedland Bernard¹,Madiwale Appasaheb N.²

Affiliation:

1. The Singer Company, Kearfott Division, Little Falls, New Jersey

2. MIT Lincoln Laboratories, Lexington, Massachusetts

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.20228

Reference11 articles.

1. ^mmert, R. I. etal. "Detailed Stability and Control Investigations of a Bank-to-Turn Configuration," AFATL-TR-78-10, Air Force Armament Laboratory, Eglin AFB, FL, Jan.1972.

2. Robustness with observers

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