INTERCEPTION OF HIGH-SPEED TARGET BY BEAM RIDER MISSILE

Author:

ELNAN ODIN R. S.1,LO HSU2

Affiliation:

1. University of Cincinnati, Cincinnati, Ohio

2. Purdue University, Lafayette, Ind.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference4 articles.

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Geometric Properties of Planar and Spherical Interception Curves;Axioms;2023-07-20

2. Beamriding Homing Systems for UAV: New Approaches and Applications;2022 IEEE 9th International Workshop on Metrology for AeroSpace (MetroAeroSpace);2022-06-27

3. SMC-Based Integrated Guidance and Control for Beam Riding Missiles With Limited LBPU;IEEE Transactions on Aerospace and Electronic Systems;2021-10

4. Integrated guidance and control system design for laser beam riding missiles with relative position constraints;Aerospace Science and Technology;2020-03

5. Inscribed-Angle Guidance Against Moving Targets;Journal of Guidance, Control, and Dynamics;2017-12

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