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2004•Unpublished venueRequires access

Real-time computation of initial optimization trajectory with quasi-Newton methods:real-time computation methods of air defence missile trajectory′s optimization

Fei Jinggao

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Abstract

Some real-time computation problems for the optimization of air defence missile trajectory are presented,and the quasi-Newton methods are used to compute the initial optimization trajectory.

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What this paper is about

Some real-time computation problems for the optimization of air defence missile trajectory are presented,and the quasi-Newton methods are used to compute the initial optimization trajectory.

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Available abstract

Some real-time computation problems for the optimization of air defence missile trajectory are presented,and the quasi-Newton methods are used to compute the initial optimization trajectory.

Key concepts: Trajectory, Computation, Trajectory optimization, Missile, Missile guidance, Computer science, Control theory (sociology), Engineering

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