Abstract
A General Purpose Flight Simulator System was installed at National Aerospace Laboratory in July of 1963. It consists of an analog computer unit, a flight table unit and a moving cockpit unit. This system is used for the research on flight performance, stability and control of aircraft and rocket, involving autostabilizer or human pilot. Various simulation studies on conventional aircraft, V/STOL aircraft and rocket are now being carried out using this system successfully.
In this paper, the system design, construction and function of each unit including various components are reported.
