Design of a Flight Envelope Protection System for NASA’s Transport Class Model-Reference-Cited by-同舟云学术

Design of a Flight Envelope Protection System for NASA’s Transport Class Model

Published:2017-04 Issue:4 Volume:40 Page:863-877
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Tekles Nikolas¹,Chongvisal June¹,Xargay Enric¹,Choe Ronald¹,Talleur Donald A.¹,Hovakimyan Naira¹,Belcastro Christine M.²

Affiliation:

1. University of Illinois at Urbana-Champaign, Urbana, Illinois 61801

2. NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.G001728

Reference26 articles.

1. EvansJ. K. “An Examination of in Flight Loss of Control Events During 1988–2004,” Alliant Techsystems, Inc. Rept. NNL07AM99T/R1C0, Hampton, VA, 2007.

2. Airplane Upsets: Old Problem, New Issues

3. Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control Accidents

4. BelcastroC. M.BelcastroC. M. “Future Research Directions for the Development of Integrated Resilient Flight Systems to Prevent Aircraft Loss-of-Control Accidents, Part 1: System Technologies,” NASA TM (to be published).

5. L1 adaptive control for safety-critical systems

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