Design and Performance of the OrbView-2 Attitude Control System
The OrbView-2 satellite, launched on August 1, 1997, is the world's first commercially owned imaging satellite. Because of the commercial nature of the mission, design of the OrbView-2 attitude control system was constrained by cost as well as the normal physical parameters. In addition to maintaining a nadir-pointing momentum-biased mission mode, the spacecraft maintains a wide variety of operating modes including an extended orbit-raising sequence. The mission requirements were met without the use of gyros or other high-cost attitude sensing hardware. This paper provides an overview of the attitude control system design as well as a description of the post-launch system performance.
Authors
- Sanjivan Sivapiragasam
- Tobin Anthony
Institutions
- Northrop Grumman (United States) (US)
Publication Details
- Journal
- Digital Commons - USU (Utah State University)
- Published
- 2025-08-07
- DOI
- https://doi.org/10.26077/saza-am72
- Primary Topic
- Inertial Sensor and Navigation
- Type
- article
Funders
- National Aeronautics and Space Administration
- Goddard Space Flight Center