Computer Programs for Computational Assistance in the Design of Aircraft Control Systems

摘要

A package of FORTRAN subroutines capable of generating aircraft transfer functions in six degrees of freedom is presented. Considerable flexibility is afforded in the specification of the reference condition and the vehicle aerodynamic, inertial, and geometric properties. The package is designed to be used with a main program defining the particular system configuration under study. The package has been prepared for use on the CDC 6600, the IBM 7090/7094, and the IBM 360 computers. The report includes program listings.