Analysis of NLR Configurations Using OCM (Optimal Control Modeling) for Pilot Modeling.

摘要

A summary of the results obtained from an analytic handling qualities analysis of the rate-command/attitude-hold aircraft configurations is presented. Pilot/vehicle performance was evaluated using an optimal control technique for pilot modeling. Numerical and graphical results for a closed-loop frequency-domain analysis are presented and discussed and comparisons with experimental results are made. Finally, the results are compared with those from another study that dealt with similar configurations.