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http://dx.doi.org/10.5302/J.ICROS.2008.14.8.824

Flight Control System Design and Verification Process  

Kim, Chong-Sup (한국항공우주산업(주))
Publication Information
Journal of Institute of Control, Robotics and Systems / v.14, no.8, 2008 , pp. 824-836 More about this Journal
Abstract
Relaxed static stability(RSS) concept has been applied to improve aerodynamic performance of modern version supersonic jet fighter aircraft. Therefore, flight control systems are necessary to stabilize an unstable aircraft, and provides adequate handling qualities and achieve performance enhancements. Standard FCSDVP (Flight Control System Design and Verification Process) is provided to reduce development period of the flight control system. In addition, if this process is employed in developing flight control system, it reduces the trial and error for development and verification of flight control system. This paper addresses the flight control system design and verification process for the RSS aircraft utilizing design goal based on military specifications, linear and nonlinear system design and verification based on universal software, handling quality test based on HILS(Hardware In-the-Loop Simulator) environment, and ground and flight test results to verify aircraft dynamic flight responses.
Keywords
FCSDVP(Flight Control System Design and Verification Process); HILS (Hardware In-the-Loop Simulator); ground and flight test; linear and nonlinear system design and verification;
Citations & Related Records
Times Cited By KSCI : 7  (Citation Analysis)
연도 인용수 순위
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