Optimal Feedback Guidance of a Small Aerial Vehicle in a Stochastic Wind-Reference-Cited by-同舟云学术

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Optimal Feedback Guidance of a Small Aerial Vehicle in a Stochastic Wind

Published:2013-07 Issue:4 Volume:36 Page:975-985
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Anderson Ross P.¹,Bakolas Efstathios²,Milutinović Dejan¹,Tsiotras Panagiotis³

Affiliation:

1. Department of Applied Mathematics and Statistics, University of California, Santa Cruz, Santa Cruz, California 95064

2. Department of Aerospace Engineering, University of Texas at Austin, Austin, Texas 78712-1221

3. School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332

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/10.2514/1.59512

Reference14 articles.

1. On Curves of Minimal Length with a Constraint on Average Curvature, and with Prescribed Initial and Terminal Positions and Tangents

2. IsaacsR. “Games of Pursuit,” RAND, Rept. No. P-257, 1951.

3. Unmanned Aerial Vehicle Path Following for Target Observation in Wind

4. Vector Field Path Following for Miniature Air Vehicles

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