Command Shaping Optimal Guidance Laws Against High-Speed Incoming Targets-Reference-Cited by-同舟云学术

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Command Shaping Optimal Guidance Laws Against High-Speed Incoming Targets

Published:2015-10 Issue:10 Volume:38 Page:2025-2033
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Ryu Moo-Yong¹,Lee Chang-Hun²,Tahk Min-Jea¹

Affiliation:

1. Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea

2. Agency for Defense Development, Daejeon 305-600, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G001131

Reference22 articles.

1. ZarchanP., Tactical and Strategic Missile Guidance, 5th ed., AIAA, Reston, VA, 2007, pp. 143–161.

2. New Proportional Navigation Law for Ground-to-Air Systems

3. BrysonA. E.Jr.HoY.C., Applied Optimal Control, Wiley, New York, 1975, pp. 154–155.

4. Ben-AsherJ. Z.YaeshI., Advanced in Missile Guidance Theory, Vol. 180, AIAA, Reston, VA, 1988, pp. 22–35.

5. Switched bias proportional navigation for homing guidance against highly maneuvering targets

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