タイトル | Multiple IMU system test plan, volume 4 |
本文(外部サイト) | http://hdl.handle.net/2060/19750004846 |
著者(英) | Whittredge, R. S.; Vincent, K. T., Jr.; Landey, M. |
著者所属(英) | Draper (Charles Stark) Lab., Inc. |
発行日 | 1974-10-01 |
言語 | eng |
内容記述 | Operating procedures for this redundant system are described. A test plan is developed with two objectives. First, performance of the hardware and software delivered is demonstrated. Second, applicability of multiple IMU systems to the space shuttle mission is shown through detailed experiments with FDI algorithms and other multiple IMU software: gyrocompassing, calibration, and navigation. Gimbal flip is examined in light of its possible detrimental effects on FDI and navigation. For Vol. 3, see N74-10296. |
NASA分類 | AIRCRAFT COMMUNICATIONS AND NAVIGATION |
レポートNO | 75N12918 R-798-VOL-4 NASA-CR-120541 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/191944 |