Accession Number : AD0514607
Title : OMEGA Feasibility Flight Test RC-135C.
Descriptive Note : Final rept.,
Corporate Author : STRATEGIC RECONNAISSANCE WING (55TH) OFFUTT AFB NEBR
Personal Author(s) : Leaver,Carl A.
Report Date : 10 FEB 1971
Pagination or Media Count : 220
Abstract : The feasibility of OMEGA as a world-wide backup navigation system for high speed, high altitude aircraft has been demonstrated. At most, minimum rate aiding from external sensors is required when OMEGA is employed under cruise vehicle dynamics. The generally predicted accuracy of 1 to 2 NM is considered conservative in view of the probability of future refinement of propagation prediction based on empirical data. Current problems resulting from poor geometry, interference, weak signal and resulting low signal-to-noise ratio will become academic with the implementation of the full power transmitter network by the end of 1973. Equipment is highly reliable, simple to operate and lends itself well to interface with other systems and the assumption of related tasks. Interference problems do not appear serious at this time. A continued effort is in order to further refine equipment and exploit such additional applications as Differential, Inertial and Retransmitted OMEGA. Full utilization of the global reconnaissance mission and environment should be exercised to permit timely and cost effective achievement of this goal. (Author)
Descriptors : (*HYPERBOLIC NAVIGATION, FLIGHT TESTING), (*DIRECTION FINDING, AIRBORNE), PHASE DETECTORS, ACCURACY, ERRORS, PHASE MEASUREMENT (U) *AERIAL RECONNAISSANCE, INERTIAL NAVIGATION, PROPAGATION, RADIO TRANSMITTERS, STRATEGIC AIR COMMAND, HIGH ALTITUDE, RADIOFREQUENCY INTERFERENCE, SIGNAL-TO-NOISE RATIO, PLANNING, SYNCHRONIZATION(ELECTRONICS), ATOMIC CLOCKS, CESIUM, LOOP ANTENNAS, AIRCRAFT ANTENNAS, VERY LOW FREQUENCY
Subject Categories : Military Intelligence
Distribution Statement : APPROVED FOR PUBLIC RELEASE