An autonomous Nimbus Doppler positioning system
Abstract
A single-pass Doppler positioning system was developed at the GSFC in support of the Nimbus-6 mission. The system was designed to satisfy the following requirements: compatibility with the PDP 11/70 minicomputer; single-pass recovery of up to 250 positions with a two-sigma accuracy of 5 km; high reliability with a minimum of human interaction; and near real-time responsiveness. The system consists of a numerical integrator which includes only the J2 term (earth flattening) of the earth's gravity field, an editing routine, a first guess algorithm, a least squares position recovery program, and a routine for generating a 95% confidence circle based on a computer covariance matrix. An analysis and quantification of the following error sources that limit system accuracy are presented: orbit error, radial aliasing, computational difficulties with overhead passes, oscillator drift, and ambiguity problems. Results of system reliability tests and sample outputs are included.
- Publication:
-
National Aerospace Meeting
- Pub Date:
- 1981
- Bibcode:
- 1981naae.meet...71G
- Keywords:
-
- Airborne/Spaceborne Computers;
- Doppler Effect;
- Nimbus 6 Satellite;
- Positioning;
- Satellite Tracking;
- Algorithms;
- Astrionics;
- Autonomy;
- Digital Integrators;
- Error Analysis;
- Least Squares Method;
- Minicomputers;
- Position Errors;
- Space Communications, Spacecraft Communications, Command and Tracking