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Phase Compensated Rate Limiters for Alleviation of Pilot-Induced Oscillations Caused by Control Surface Rate Limiting

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Kendall, Eric R., author.
Conference Name:
Aerospace Technology Conference & Exposition (2005-10-03 : Grapevine, Texas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2005
Summary:
The basic characteristics of Phase Compensated Rate Limiters, PCRL's, are explained and their application to the alleviation of Pilot-Induced Oscillations, PIO, caused by control surface actuator rate limiting is demonstrated.It is shown that PCRL's can recover a large percentage of the control system phase loss caused by surface rate limiting while maintaining minimal temporary bias in the control surface response following rapid command reversals.Their superior performance in meeting PIO criteria is shown by comparing the simulation results from an extensive study that was aimed at finding solutions for alleviating roll-axis PIO on an airplane where aileron and spoiler surface rate limiting appeared to be a predominant causal factor.A comprehensive investigation of the effect of rate limiting in pilot-induced oscillations is reported in Ref. 2
Notes:
Vendor supplied data
Publisher Number:
2005-01-3418
Access Restriction:
Restricted for use by site license

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