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Method and apparatus for rate integration supplement for attitude referencing with quaternion differencing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 2002 |
| Description | A control system for providing attitude control in spacecraft. The control system comprising a primary attitude reference system, a secondary attitude reference system, and a hyper-complex number differencing system. The hyper-complex number differencing system is connectable to the primary attitude reference system and the secondary attitude reference system. |
| File Size | 744449 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080004972 |
| Archival Resource Key | ark:/13960/t6353m55b |
| Language | English |
| Publisher Date | 2002-09-24 |
| Access Restriction | Open |
| Subject Keyword | Astrodynamics Spacecraft Control Attitude Inclination Patents Attitude Control Quaternions Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |