Optimal Setting of the Proportional-Navigation Gain-Reference-Cited by-同舟云学术

Optimal Setting of the Proportional-Navigation Gain

Published:2013-05 Issue:3 Volume:36 Page:887-890
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Heller Carmit¹,Yaesh Isaac¹,Ben-Asher Joseph Z.²

Affiliation:

1. Head of Control Department, Israel Military Industries, 47100 Ramat-HaSharon, Israel

2. Faculty of Aerospace Engineering, Technion–Israel Institute of Technology, 32000 Haifa, Israel

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/10.2514/1.59226

Reference5 articles.

1. BrysonA. E.HoY.C., Applied Optimal Control, John Wiley & Sons, New York, 1975, pp. 153–155, 287–288.

2. ZarchanP., Tactical and Strategic Missile Guidance, edited by SeebassA. R., Vol. 124, Progress in Astronautics and Aeronautics, AIAA Inc., Washington, DC, 1990, pp. 135–145, Chap. 7.

3. The maximum amplitude cost functional in linear systems

4. Minimax frequency domain performance and robustness optimization of linear feedback systems

5. LeeE. B.MarkusL., Foundations of Optimal Control Theory, Krieger, Malabar, FL, 1986, pp. 216–217.

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