Seeker Based Optimal Guidance Law, A Few Issues
Author:
Affiliation:
1. Defence Research and Development Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5794
Reference21 articles.
1. Adaptive Radome Compensation Using Dither
2. Miss distance dynamics in homing missiles
3. Missile guidance design tradeoffs for high-altitude air defense
4. Zarchan, P. "Tactical and Strategic Missile Guidance", 3rdEdition, pp.155-159, Volume-176,Progressin Astronautics&Aeronautics,1997.
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