Research of Optimal End Guidance Law about Homing UAV

Shao Song Wan; Jian Cao; Cong Yan

doi:10.4028/www.scientific.net/AMM.415.30

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 415Research of Optimal End Guidance Law about Homing...

Research of Optimal End Guidance Law about Homing UAV

Abstract:

This paper researches optimal end guidance law about homing UAV. After building mathematic model, simulation results show that optimal end guidance law (OEGL) attacking fixed targets is superior to constant coefficient proportion guidance law (CCPGL).

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Periodical:

Applied Mechanics and Materials (Volume 415)

Pages:

30-33

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.415.30

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Online since:

September 2013

Authors:

Shao Song Wan, Jian Cao, Cong Yan

Keywords:

Guidance, Homing UAV, Mathematics Model, Simulation

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