Design, Development and Flight Testing of Control Laws for the Indian Light Combat Aircraft-Reference-Cited by-同舟云学术

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Design, Development and Flight Testing of Control Laws for the Indian Light Combat Aircraft

Published:2002-06-25 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
language:
Short-container-title:

Author:

Chetty Shyam¹,Deodhare Girish²,Misra B.³

Affiliation:

1. National Aerospace Laboratories

2. Centre for Artificial Intelligence and Robotics

3. Aeronautical Development Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-4649

Reference8 articles.

1. Design of Notch Filters for Structural Responses with Multiaxis Coupling

2. "USAF Military Standard on Flying Qualities of PilotedAircraft",MIL-STD-1797A,30 Jan.1990.

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