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Dynamics and Adaptive Control for Stability Recovery of Damaged AircraftThis paper presents a recent study of a damaged generic transport model as part of a NASA research project to investigate adaptive control methods for stability recovery of damaged aircraft operating in off-nominal flight conditions under damage and or failures. Aerodynamic modeling of damage effects is performed using an aerodynamic code to assess changes in the stability and control derivatives of a generic transport aircraft. Certain types of damage such as damage to one of the wings or horizontal stabilizers can cause the aircraft to become asymmetric, thus resulting in a coupling between the longitudinal and lateral motions. Flight dynamics for a general asymmetric aircraft is derived to account for changes in the center of gravity that can compromise the stability of the damaged aircraft. An iterative trim analysis for the translational motion is developed to refine the trim procedure by accounting for the effects of the control surface deflection. A hybrid direct-indirect neural network, adaptive flight control is proposed as an adaptive law for stabilizing the rotational motion of the damaged aircraft. The indirect adaptation is designed to estimate the plant dynamics of the damaged aircraft in conjunction with the direct adaptation that computes the control augmentation. Two approaches are presented 1) an adaptive law derived from the Lyapunov stability theory to ensure that the signals are bounded, and 2) a recursive least-square method for parameter identification. A hardware-in-the-loop simulation is conducted and demonstrates the effectiveness of the direct neural network adaptive flight control in the stability recovery of the damaged aircraft. A preliminary simulation of the hybrid adaptive flight control has been performed and initial data have shown the effectiveness of the proposed hybrid approach. Future work will include further investigations and high-fidelity simulations of the proposed hybrid adaptive Bight control approach.
Document ID
20060053343
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Nguyen, Nhan
(NASA Ames Research Center 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)
Nespeca, Pascal
(California Univ. Davis, CA, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2006
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: AIAA Guidance, Navigation, and Control Conference
Location: Keystone, CO
Country: United States
Start Date: August 20, 2006
End Date: August 24, 2006
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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