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Stall Recovery Guidance Algorithms Based on Constrained Control ApproachesAircraft loss-of-control, in particular approach to stall or fully developed stall, is a major factor contributing to aircraft safety risks, which emphasizes the need to develop algorithms that are capable of assisting the pilots to identify the problem and providing guidance to recover the aircraft. In this paper we present several stall recovery guidance algorithms, which are implemented in the background without interfering with flight control system and altering the pilot's actions. They are using input and state constrained control methods to generate guidance signals, which are provided to the pilot in the form of visual cues. It is the pilot's decision to follow these signals. The algorithms are validated in the pilot-in-the loop medium fidelity simulation experiment.
Document ID
20160000934
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Stepanyan, Vahram
(University Affiliated Research Center (Calif. Univ. Santa Cruz) Moffett Field, CA, United States)
Krishnakumar, Kalmanje
(NASA Ames Research Center Moffett Field, CA United States)
Kaneshige, John
(NASA Ames Research Center Moffett Field, CA United States)
Acosta, Diana
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
January 19, 2016
Publication Date
January 4, 2016
Subject Category
Aircraft Stability And Control
Computer Programming And Software
Report/Patent Number
ARC-E-DAA-TN24296
Meeting Information
Meeting: AIAA Science and Technology Forum and Exposition
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS2-03144
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Aircraft stall
Pilot visual cueing
Recovery guidance algorithm
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