New Structure for an Aerodynamic Fin Control System for Tail Fin-Controlled STT Missiles-Reference-Cited by-同舟云学术

New Structure for an Aerodynamic Fin Control System for Tail Fin-Controlled STT Missiles

Published:2011-10 Issue:4 Volume:24 Page:505-510
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Kim Seung-Hwan¹²³,Lee Yong-In¹²³,Tahk Min-Jea¹²³

Affiliation:

1. Ph.D. Candidate, Dept. of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon, Korea (corresponding author).

2. Ph.D. Candidate, Dept. of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon, Korea.

3. Professor, Dept. of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon, Korea.

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.1943-5525.0000088

Reference4 articles.

1. A chronological bibliography on saturating actuators

2. Flight Control System Design with Rate Saturating Actuators

3. Lu Bei Wu Fen and Kim SungWan (2003). “Linear-parameter-varying antiwindup compensation for enhanced flight control performance.” Proc. Guidance Navigation and Control Conf. AIAA Austin TX.

4. Electromechanical flight actuators for advanced flight vehicles

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