In this paper, an integrated control problem is investigated for the Air-breathing hypersonic vehicle (AHSV). The coupling dynamic model of AHSV is first provided by the Quasi One-dimensional flow theory, and the mechanical properties is analyzed. Furthermore, the integrated guidance and control laws are presented based on the proposed model and analysis result. Finally, the comparison simulation results show that the proposed integrated control approach has the better control performance against the decoupled control approach.
An Integrated Control Approach for Air-breathing Hypersonic Vehicle
2020-11-27
616756 byte
Conference paper
Electronic Resource
English
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