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《Flight Dynamics》 2009-06
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Optimal Orbital Transfer with Finite Thrust Based on Gauss Pseudospectral Method

ZHANG Ya-feng,HE Xing-suo(School of Mechanics,Civil Engineering and Architectures,Northwest Polytechnical University,Xi'an 710072,China)  
An optimal control problem based on universal variable is studied.Based on the dynamics equations with the orbital nonsingular elements,perturbation equations including universal variable for solving conic orbit are established.The optimal control problem of the equations is solved using Gauss pseudospectral method.At last,example of orbital transfer with zero inclination is computed and simulated.The simulation results demonstrate that the equations established and the Gauss pseudospectral method used in this paper are practical and can meet various constraint conditions.Gauss pseudospectral method is not sensitive to orbital transfer initial conditions and the engine easy to control.
【Fund】: 国家863计划资助项目(2007AA704308)
【CateGory Index】: V448.2
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【Co-citations】
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