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An approach to attitude determination for a spin-stabilized spacecraft (imp 1)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Fang, A. C. |
| Copyright Year | 1972 |
| Description | The analysis and the FORTRAN program are presented for the determination of attitude of a spin-stabilized spacecraft. The use of telemetry data that provide information about two reference vectors and their relation to the spin is outlined. A technique for the determination of the spin-axis orientation that employs only simple calculations is described. |
| File Size | 969837 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720023242 |
| Archival Resource Key | ark:/13960/t7rn7xf55 |
| Language | English |
| Publisher Date | 1972-08-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Explorer 18 Satellite Linear Equations Telemetry Spin Stabilization Attitude Indicators Satellite Orientation Computer Programs Fortran Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
