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Stability Properties and Cross Coupling Performance of the Control Allocation Scheme CAPIOThis paper presents a stability analysis and an application of a recently developed Control Allocator for recovery from Pilot Induced Oscillations (CAPIO). When actuators are rate-saturated due to either aggressive pilot commands, high gain ight control systems or some anomaly in the system, the effective delay in the control loop may increase. This effective delay increase manifests itself as a phase shift between the commanded and actual system signals and can instigate Pilot induced Oscillations (PIO). CAPIO reduces the e ective time delay by minimizing the phase shift between the commanded and the actual attitude accelerations. We present a stability analysis of CAPIO for a scalar system. In addition, we present simulation results for aircraft with cross-coupling which demonstrates the potential of CAPIO serving as an effective PIO handler in adverse conditions.
Document ID
20100027543
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Yildiz, Yildiray
(California Univ. Santa Cruz, CA, United States)
Kolmanovsky, Ilya V.
(Ford Motor Co. Dearborn, MI, United States)
Date Acquired
August 24, 2013
Publication Date
April 20, 2010
Subject Category
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN1308
Report Number: ARC-E-DAA-TN1308
Meeting Information
Meeting: AIAA Infotech@Aerospace
Location: Atlanta, GA
Country: United States
Start Date: April 20, 2010
End Date: April 22, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
TASK: TO.056.9.DA.TI
CONTRACT_GRANT: NAS2-03144
Distribution Limits
Public
Copyright
Public Use Permitted.
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