An Integrated Control Approach for Air-breathing Hypersonic Vehicle

Abstract

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.