Abstract
This paper provides a mathematical formulation and two solution algorithms of the problem of spacecraft spin axis attitude determination from noisy measurements. The two developed algorithms are compared through digital simulation and their relative merits in terms of estimation accuracy and computational requirements are discussed.
| Original language | English |
|---|---|
| Pages (from-to) | 529-534 |
| Number of pages | 6 |
| Journal | IEEE Transactions on Aerospace and Electronic Systems |
| Volume | 28 |
| Issue number | 2 |
| DOIs | |
| State | Published - Apr 1992 |
ASJC Scopus subject areas
- Aerospace Engineering
- Electrical and Electronic Engineering