An iterative method is presented for determining the position on earth of a balloon, correcting for both errors due to terrestrial rotation and errors due to the Doppler effect. An interrogating satellite is used, and a zero wind condition is assumed. The accuracy obtained is on the order of 1 millionth.
Errors Due to Terrestrial Rotation. Errors Due to Inherent Balloon Speed. Complete Restitution of Localization (Doppler)
1972
33 pages
Report
Keine Angabe
Englisch