NASA NTRS ยท 19830011216
A system study for the application of microcomputers to research flight test techniques
Abstract
The onboard simulator is a three degree of freedom aircraft behavior simulator which provides parameters used by the interception procedure. These parameters can be used for verifying closed loop performance before flight. The air to air intercept mode is a software package integrated in the simulation process that generates a target motion and performs a tracking procedure that predicts the most likely next target position, for a defined time step. This procedure also updates relative position parameters and gives adequate fire commands. A microcomputer based on an aircraft spin warning system periodically samples the assymetric thrust and yaw rate of an airplane and then issues voice synthesized warnings and /or suggests to the ilot how to respond to the situation.
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Smyth, R. K.. 1983-01-01. A system study for the application of microcomputers to research flight test techniques. https://ntrs.nasa.gov/citations/19830011216
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