Numerical solutions of Hamiltonian DAE’s and applications

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In this paper, we present a numerical method for nonlinear differential algebraic equations (DAE’s) based on the backward differential formulas (BDF) and the Padé series. Usefulness of the method is then illustrated by a numerical example, which is concerned with the derivation of the optimal guidance law for spacecraft. We will reformulate the problem as a Hamiltonian DAE system. After establishing the system of spacecraft dynamics, we can derive the optimal guidance law of the system by numerical method.

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论文评审过程:Available online 25 January 2006.

论文官网地址:https://doi.org/10.1016/j.amc.2005.11.147