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NASA NTRS · 19760023114

Real time flight simulation methodology

Abstract

An example sensitivity study is presented to demonstrate how a digital autopilot designer could make a decision on minimum sampling rate for computer specification. It consists of comparing the simulated step response of an existing analog autopilot and its associated aircraft dynamics to the digital version operating at various sampling frequencies and specifying a sampling frequency that results in an acceptable change in relative stability. In general, the zero order hold introduces phase lag which will increase overshoot and settling time. It should be noted that this solution is for substituting a digital autopilot for a continuous autopilot. A complete redesign could result in results which more closely resemble the continuous results or which conform better to original design goals.

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BibTeXRIS

Parrish, E. A., Cook, G., Mcvey, E. S.. 1976-08-01. Real time flight simulation methodology. https://ntrs.nasa.gov/citations/19760023114

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