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- W1571335469 abstract "The contributions to nonlinear behavior and unstable response of the model following yaw control system of a VTOL aircraft during hover were determined. The system was designed as a state rate feedback implicit model follower that provided yaw rate command/heading hold capability and used combined full authority parallel and limited authority series servo actuators to generate an input to the yaw reaction control system of the aircraft. Both linear and nonlinear system models, as well as describing function linearization techniques were used to determine the influence on the control system instability of input magnitude and bandwidth, series servo authority, and system bandwidth. Results of the analysis describe stability boundaries as a function of these system design characteristics." @default.
- W1571335469 created "2016-06-24" @default.
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- W1571335469 date "1982-03-01" @default.
- W1571335469 modified "2023-09-26" @default.
- W1571335469 title "An analysis of a nonlinear instability in the implementation of a VTOL control system" @default.
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- W1571335469 hasPublicationYear "1982" @default.
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