2004•Unpublished venueRequires access

Gradient projection descent algorithms for real-time computation of trajectory optimization:real-time computation methods for optimization of air defence missile trajectory II

Fei Jinggao

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Abstract

In the execution of launch of the air defence missie,it is needed within a fixed response time to determine the optimal trajectory,along which the missile flies through the predictive rendezvous at the predictive time.The gradient projection algorithms are constructed for the real-time computation of trajectory optimization,and the concrete steps of the algorithms are also given.The digital simulation results for a mathematical model of motion of the air defence missile show that the sufficient high control accuracy can be achieved with these algorithms.

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What this paper is about

In the execution of launch of the air defence missie,it is needed within a fixed response time to determine the optimal trajectory,along which the missile flies through the predictive rendezvous at the predictive time.The gradient projection algorithms are constructed for the real-time computation of trajectory optimization,and the concrete steps of the algorithms are also given.The digital simulation results for a mathematical model of motion of the air defence missile show that the sufficient high control accuracy can be achieved with these algorithms.

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Available abstract

In the execution of launch of the air defence missie,it is needed within a fixed response time to determine the optimal trajectory,along which the missile flies through the predictive rendezvous at the predictive time.The gradient projection algorithms are constructed for the real-time computation of trajectory optimization,and the concrete steps of the algorithms are also given.The digital simulation results for a mathematical model of motion of the air defence missile show that the sufficient high control accuracy can be achieved with these algorithms.

Key concepts: Trajectory, Missile, Trajectory optimization, Computation, Descent (aeronautics), Rendezvous, Gradient descent, Computer science

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