DocumentCode
1409445
Title
Use of satellites for navigation
Author
Chu, Juo-Wen
Author_Institution
Aeronautics Navigation Services and Maintenance Office, CAA, Taipei, Taiwan, Republic of China
Issue
5
fYear
1968
Firstpage
799
Lastpage
800
Abstract
Any position on earth can be determined as the intersection of two circles, with their centers located at 0 and 0´ on the earth´s surface just beneath two satellites. Therefore any flying path can be described as a locus of many such positions. One synchronous satellite can cover 45 percent of the surface of the earth. When an aircraft flies outbound along the earth´s surface from the reference point 0, the traveling time of the wave pulses transmitted from the satellite to the aircraft becomes longer and longer, but it is not proportional to the flying distance, because the altitude angle (the intersection angle between the line from the satellite to the measured point and the tangent line to the earth´s surface at the point) changes from time to time. The increase of the transit time will be less when flying the same distance over the area near the reference point than it would be farther away. A correction factor cos(90-α-β) should be introduced to equalize the measured distance to the true flying distance.
Keywords
Earth; Frequency synchronization; Position measurement; Pulse generation; Pulse measurements; Satellite navigation systems;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1968.5408698
Filename
5408698
Link To Document