首页 | 本学科首页   官方微博 | 高级检索  
     


Nonlinear time-domain models of human controllers
Authors:Lawrence W. Taylor Jr.
Affiliation:(1) NASA-Flight Research Center, Edwards, California
Abstract:Data from a compensatory tracking task are analyzed by using time-domain models. The linear time-domain results are transformed and compared with frequency-domain results. The nonlinear time-domain model of the same data reduced the remnant or residual power by only a small amount. The need for testing models on independent data is discussed. A novel, but attractive, method of generating functions for an efficient functional expansion of time-domain models is offered.Notation c Pilot output (control deflection), inches - E Error matrix - e Error, radians - F[·] Fourier transform - h Time interval, seconds - hi Sample of impulse response of pilot - hp Impulse response of pilot, inches/radian or inches/degree - i Input (external disturbance function), radians - M Maximum value ofm, M=TM/Deltatau - m Index for the argument ofhp - N Maximum value ofn - n Index for time - o Linear output of pilot model (control deflection), inches - r Remnant signal of pilot model (control deflection), inches - S Matrix - s Laplace variable - TM Maximum memory time of the pilot model, seconds - t Time, seconds - Yc Transfer function of controlled element - Ycjohgr) Controlled-element transfer function, radians/inch - Ypjohgr) Pilot-describing function, inches/radian - tau Argument ofhp, seconds - Deltatau Incremental value oftau, seconds - ohgr Frequency, radians/second - ^ Estimate - par Absolute value - ang Phase angle
Keywords:
本文献已被 SpringerLink 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号