ORBIT DETERMINATION FROM SIMULTANEOUS RADIO DOPPLER-SHIFT MEASUREMENTS
Abstract
A method of computing th orbit of a satellite from radio Doppler shift measurements is described. It is assumed that radio signals originate at a transmitter on the ground, are reflected by a satellite and received at three receivers during the same pass of the satellite over the area in which the four stations are located. Examples of orbit computations are given. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1961
- Accession Number
- AD0266084
Entities
People
- Ceslovas Masaitis
- Michael J. Romanelli
Organizations
- Ballistic Research Laboratory