Incorporation of the Six Dimensional, Linearized Equations of Motion with a Variable Stability Flight Simulator.
NAVAL POSTGRADUATE SCHOOL MONTEREY CALIF
Pagination or Media Count:
In this report the equations of motion for the six degrees of freedom of an aircraft were solved by an analog computer circuit. These solutions were incorporated with the instrumentation of a fixed base flight simulator to provide a variable stability aircraft demonstration device. Author
- Test Facilities, Equipment and Methods