This paper describes a study of those aspects of Omega navigationthat are unique to aircraft applications. The main effort of the studyis to use a digital computer to simulate the reception of Omega signals.Three principal conclusions are drawn: the poorer signal-to-noiseratio environment will not preclude reception; interfering carriers willnot preclude reception; and the required velocity-aiding accuracy isquite modest in terms of that which is readily available from inertialsystems.
Aircraft Navigation Using Omega
IEEE Transactions on Aerospace and Electronic Systems ; AES-5 , 5 ; 756-761
1969-09-01
1828900 byte
Article (Journal)
Electronic Resource
English
Engineering Index Backfile | 1962
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