28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-5.7.1
RESEARCH ON OPTIMIZING ASCENT TRAJECTORY OF AERO-SPACE PLANE BASED ON COMBINED CYCLE PROPULSION
Z. X. Yao
Shenyang Aircraft Design and Research Inst., China
Keywords: aero-space, ascent optimization
It is established that the flight dynamics model of the ASP which can take off and land horizontally, and flight at hypersonic. The flow chart of optimizing the ASPís climb trajectory is designed by adjusting some parameters of flight-path angle, angle of attack, mode of turbine and rocket-ramjet engine.
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