CONVERSION FROM THE BASIC MEASUREMENTS OF A 'RANGE ONLY' TRACKING SYSTEM TO RECTANGULAR COORDINATES
Abstract
The method used here is that of obtaining the rectangular coordinates of three trackers with respect to a coordinate system whose x y plane is tangent to an ellipsoidal earth at the location of one of the trackers. Attention is called to the fact that the calculations for this are executed prior to any real time computations. After this is accomplished it is analytically simple to solve three distance equations in three unknowns to obtain the rectangular coordinates of the missile. Complete procedures are given in the text.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 19, 1959
- Accession Number
- AD0834063
Entities
People
- A. Saastad
Organizations
- General Dynamics