Description of gyroscopes and accelerometers suitable for navigational purposes; principles involved in inertial navigation round earth are explained; it is shown that pure inertial system is undamped, that introduction of damping leads to system errors, but that these can be eliminated by use of velocity measurement from Doppler system; advantages of combination of Doppler and inertial systems; comparison of individual and combined systems.
Aircraft inertial navigation
Aircraft Eng
Aircraft Engineering ; 36 , n 1
1964
8 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
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