Missile trajectory optimization with agility issues-Reference-Cited by-同舟云学术

Missile trajectory optimization with agility issues

Published:1996-07-29 Issue: Volume: Page:
ISSN:
Container-title:Guidance, Navigation, and Control Conference
language:
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Author:

Nasuti Francesco¹,Innocenti Mario¹

Affiliation:

1. Pisa, Univ., Italy

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3730

Reference11 articles.

1. North Atlantic Treaty Organization: AGARDAR-314. "Operational Agility", Technical Report of WorkingGroupFMP19,1994.

2. Innocenti, M. "Integrated Approachto Guidance and Control of Alternate Control Technology Flight Vehicles," Annual Technical Report: ATR-1, Grant: F08630-94-1-0001, Air Force Material Command, WL/MNAV, Eglin AFB, 52342 Florida, November 21,1995

3. Bruns, K.D., and others, "Missile DATCOM", WL-TR-91-3039.

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