Optimal Impact Angle Control Guidance Law Based on Linearization About Collision Triangle-Reference-Cited by-同舟云学术

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Optimal Impact Angle Control Guidance Law Based on Linearization About Collision Triangle

Published:2014-05 Issue:3 Volume:37 Page:958-964
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Cho Hangju¹,Ryoo Chang-Kyung²,Tsourdos Antonios³,White Brian³

Affiliation:

1. Hanwha Corporation Research and Development Center, Daejeon 305-156, Republic of Korea

2. Department of Aerospace Engineering, Inha University, Incheon 402-751, Republic of Korea

3. Defence Academy of the United Kingdom, Cranfield University, Shrivenham, England SN6 8LA, United Kingdom

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/10.2514/1.62910

Reference12 articles.

1. Adaptive Terminal Guidance for Hypervelocity Impact in Specified Direction

2. Generalized Vector Explicit Guidance

3. Guidance Law Design for Missiles with Reduced Seeker Field-of-View

4. BrysonE. A.HoY.C., Applied Optimal Control (rev. printing), Hemisphere, Washington, D.C., 1975, pp. 158–167.

5. ZarchanP., Tactical and Strategic Missile Guidance, 4th ed., AIAA, Reston, VA, 2002, pp. 20–28.

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