Angle of attack guidance via robust approximate inversion-Reference-Cited by-同舟云学术

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Angle of attack guidance via robust approximate inversion

Published:1998-08-10 Issue: Volume: Page:
ISSN:
Container-title:Guidance, Navigation, and Control Conference and Exhibit
language:
Short-container-title:

Author:

Innocenti Mario¹,Carnasciali Gianluca¹,Nasuti Francesco¹

Affiliation:

1. Pisa, Univ., Italy

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-4113

Reference11 articles.

1. Fundamentals of proportional navigation

2. [2]Cloutier, J.R.,Evers, J.H., Feeley, J.J. "AssessmentofAir-to-AirMissileGuidanceand Control Technology", IEEE Control Systems Magazine, October 2989,pp.27-34.

3. AIAA-98-4113

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. Nonlinear guidance techniques for agile missiles;Control Engineering Practice;2001-10

2. All-aspect acceleration-limited homing guidance;Guidance, Navigation, and Control Conference and Exhibit;1999-08-09

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