On Determining the Plane of an Artificial Satellite's Orbit.
Abstract
The problem of rapidly and accurately determining the orbital plane of an artificial earth satellite from a short series (< or = 10 superscript m) of observations is posed and solved. The observations can be either angles only data or angles and angular rates. The accuracy is generally 5 deg. In addition, another look is given to the angular velocity distance estimation technique. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 02, 1979
- Accession Number
- ADA066248
Entities
People
- Laurence G. Taff
Organizations
- Massachusetts Institute of Technology