Incorporation of Flight Control Design Tools into the Multi-Disciplinary Conceptual Design Process-Reference-Cited by-同舟云学术

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Incorporation of Flight Control Design Tools into the Multi-Disciplinary Conceptual Design Process

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Takahashi Timothy¹,Fanciullo Todd¹,Ridgely D.¹

Affiliation:

1. Raytheon Missile Systems

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-656

Reference12 articles.

1. A Generic Guidance and Control Structure for Six-Degree-of-Freedom Conceptual Aircraft Design

2. A Generic Stability and Control Methodology for Novel Aircraft Conceptual Design

3. 5Beaufrere, H. "Handbook of Control Power Requirements for Statically Unstable AircraftCoupling Dynamics in Aircraft, A Historical Perpective," Tech. rep., USAF Report F33615-84-C-3604, Jun 1997.

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1. Design Methodology of a Mini-Missile Considering Flight Performance and Guidance Precision;Journal of Systems Engineering and Electronics;2024-02

2. The Role of Guidance, Navigation, and Control in Hypersonic Vehicle Multidisciplinary Design and Optimization;16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference;2009-06-14

3. External Geometry Optimization with Flight Mechanics Constraints Using Response Surfaces;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2008-06-15

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