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http://dx.doi.org/10.5139/IJASS.2015.16.2.137

Compromise Optimal Design using Control-based Analysis of Hypersonic Vehicles  

Liu, Yanbin (College of Astronautics, Nanjing University of Aeronautics and Astronautics)
bing, Hua (College of Astronautics, Nanjing University of Aeronautics and Astronautics)
Publication Information
International Journal of Aeronautical and Space Sciences / v.16, no.2, 2015 , pp. 137-147 More about this Journal
Abstract
Hypersonic vehicles exhibit distinct dynamic and static characteristics, such as unstable dynamics, strict altitude angle limitation, large control bandwidth, and unconventional system sensitivity. In this study, compromise relations between the dynamic features and static performances for hypersonic vehicles are investigated. A compromise optimal design for hypersonic vehicles is discussed. A parametric model for analyzing the dynamic and static characteristics is established, and then the optimal performance indices are provided according to the different design goals. A compromise optimization method to balance the dynamic and static characteristics is also discussed. The feasibility of this method for hypersonic vehicles is demonstrated.
Keywords
Hypersonic Vehicles; Compromise Optimal Design; Dynamic Characteristics; Flight Stability; Parametric Model;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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