File:ST-124gimbals.jpg
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DescriptionST-124gimbals.jpg |
English: The ST-124-M3 has three gimbals, of which the outermost is attached to the Instrument Unit and the innermost is fixed in inertial space. As the vehicle rolls, pitches and yaws during flight and orbit the inner gimbal remains oriented toward the same point in space at which it was pointed at the moment of launch. The inner gimbal carries accelerometers which measure vehicle accelerations in this fixed, inertial coordinate system. Three gyros also attached to the inner gimbal sense any rotations of this gimbal and send signals to feedback circuits which drive servotorque motors that counter the rotations by nulling the gyro outputs. The resolvers measure the angles of the three gimbals, providing the attitude data of the vehicle to the navigation system. The prisms are part of the system for aligning the inner gimbal just before launch. |
Date | |
Source | Marshall Space Flight Center (1 November 1968) Astrionics System Handbook - Saturn Launch Vehicles, NASA, p. p. 14.2−2 NASA-CR-102371, MSFC-IV-4-401-1, IBM-68-996-0002 |
Author | NASA/MSFC |
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Public domain |
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Public domainPublic domainfalsefalse |
This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.) | ||
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Original upload log edit
The original description page was here. All following user names refer to en.wikipedia.
- 2007-06-15 22:27 EdgarDurbin 1816×1887× (386163 bytes) Diagram of ST-124 gimbals. The ST-124-M3 has three gimbals, of which the outermost is attached to the Instrument Unit and the innermost is fixed in inertial space. As the vehicle rolls, pitches and yaws during flight and orbit the inner gimbal remains or
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current | 08:55, 24 October 2011 | 1,816 × 1,887 (377 KB) | Huntster (talk | contribs) | == {{int:filedesc}} == {{Information |Description={{en|1=The ST-124-M3 has three gimbals, of which the outermost is attached to the Instrument Unit and the innermost is fixed in inertial space. As the vehicle rolls, pitches and yaws during flight and orbi |
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Orientation | Normal |
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Horizontal resolution | 300 dpi |
Vertical resolution | 300 dpi |
Software used | Adobe Photoshop CS Macintosh |
File change date and time | 21:33, 23 September 2004 |
Color space | Uncalibrated |
Image width | 1,816 px |
Image height | 1,887 px |
Date and time of digitizing | 17:30, 23 September 2004 |
Date metadata was last modified | 17:33, 23 September 2004 |