Cooperative Optimal Guidance Laws for Imposing a Relative Intercept Angle-Reference-Cited by-同舟云学术

Cooperative Optimal Guidance Laws for Imposing a Relative Intercept Angle

Published:2015-08 Issue:8 Volume:38 Page:1395-1408
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Shaferman Vitaly¹,Shima Tal²

Affiliation:

1. Institute of Automation and Control, Vienna University of Technology, 1040 Vienna, Austria

2. Dept. 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.G000568

Reference30 articles.

1. Cooperative Multiple-Model Adaptive Guidance for an Aircraft Defending Missile

2. ShafermanV. “Cooperative Tracking and Guidance for Autonomous Aerial Vehicles”, Ph.D. Dissertation, Technion–Israel Inst. of Technology, Haifa, Israel, 2011.

3. Terminal Guidance for Impact Attitude Angle Constrained Flight Trajectories

4. Optimal Guidance Laws with Terminal Impact Angle Constraint

5. Time-to-go weighted optimal guidance with impact angle constraints

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