Flight simulation for an inertial navigation system
Abstract
Kinematic schemes and control laws are developed for testing an inertial navigation system using a dynamic flight simulator. The inertial navigation system considered here consists of two accelerometers mounted on a gyrostabilized platform which is absolutely free in the azimuth. Control laws for simulating both the ideal and the perturbed operation of the inertial navigation system are obtained. The possibility of flight simulation for a three-accelerometer inertial navigation system is also discussed.
- Publication:
-
Moskovskii Universitet Vestnik Seriia Matematika Mekhanika
- Pub Date:
- August 1983
- Bibcode:
- 1983MVSMM.......95A
- Keywords:
-
- Control Simulation;
- Dynamic Control;
- Flight Control;
- Flight Simulation;
- Inertial Navigation;
- Accelerometers;
- Control Stability;
- Gyrostabilizers;
- Space Navigation;
- Space Communications, Spacecraft Communications, Command and Tracking