Near-Optimal Missile Avoidance Trajectories via Receding Horizon Control-Reference-Cited by-同舟云学术

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Near-Optimal Missile Avoidance Trajectories via Receding Horizon Control

Published:2006-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
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Author:

Karelahti Janne¹,Virtanen Kai¹,Raivio Tuomas¹

Affiliation:

1. Helsinki University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6312

Reference43 articles.

1. 1Shaw, R. L., Fighter Combat: Tactics and Maneuvering, Naval Institute Press, Annapolis, MD, 1985, pp.46-48, 58-60.

2. Near-Optimal Flight Trajectories Generated by Neural Networks

3. Robust Optimal Onboard Reentry Guidance of a Space Shuttle: Dynamic Game Approach and Guidance Synthesis via Neural Networks

4. Model predictive control: Theory and practice—A survey

5. Introduction to Model Based Predictive Control

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Game Theoretic Strategies for Intercepting Intelligent Cruise Missiles;AIAA Guidance, Navigation and Control Conference and Exhibit;2007-06-15

2. Inverse Flight Simulation Using Aircraft Performance Models;AIAA Modeling and Simulation Technologies Conference and Exhibit;2006-06-15

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