Modified Command to Line-of-Sight Intercept Guidance for Aircraft Defense-Reference-Cited by-同舟云学术

Modified Command to Line-of-Sight Intercept Guidance for Aircraft Defense

Published:2013-05 Issue:3 Volume:36 Page:898-902
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Yamasaki Takeshi¹,Balakrishnan S. N.²,Takano Hiroyuki³

Affiliation:

1. Dept. of Aerospace Engineering, National Defense Academy of Japan, Kanagawa 239-8686, Japan

2. Dept. of Mechanical and Aerospace Engineering, Missouri University of Science and Technology, Rolla, Missouri 65409

3. Dept. of Aerospace Engineering, National Defense Academy of Japan, Kanagawa, 239-8686, Japan

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/10.2514/1.58566

Reference17 articles.

1. Progress in Astronautics and Aeronautics;Zarchan P.,2007

2. Modeling and Simulation of Aerospace Vehicle Dynamics, Second Edition

3. BrysonA. E.Jr.HoY.C., Applied Optimal Control: Optimization, Estimation, and Control, Hemisphere Publishing Corporation, New York, 1975, pp. 154–155.

4. Optimal guidance for acceleration constrained missile and maneuvering target

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