| |
| | GUIDANCE, NAVIGATION AND CONTROL |
 | | Navigation aids on board the orbiter include the three inertial measurement units, three tactical air navigation units, two air data probe assemblies, three microwave scan beam landing systems and two radar altimeters. |
 | | The inertial stability of the spin axis is a basic property of gyroscopes and is used in stabilization loops, which consist of the gyro pick-off, gimbals and gimbal torquers. |
 | | Since the navigation base provides the mount for the IMUs and star trackers, the star tracker line of sight is referenced to the navigation base and the orbiter coordinate system; thus, the GPC knows where the star tracker is pointed and its orientation with respect to the IMUs. |
| science.ksc.nasa.gov /shuttle/technology/sts-newsref/sts-gnnc.html (11375 words) |
|