Fundamentals of inertia navigation and measurement of acceleration required by means of force feed-back accelerometer; in place of separate accelerometer and integrator, many systems use integrating gyro accelerometer which measures speed directly; types of gyroscopes; detailed design of inertia navigation system will depend on operational requirements of missile; example of Thor navigation system.
Inertial navigation
Aeroplane Astronautics
Aeroplane and Astronautics ; 98 , n 2536
1960
4 pages
Aufsatz (Zeitschrift)
Englisch
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