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Summary
| Description |
English: Apollo Inertial Measurement Unit, where Inertial Reference Integrating Gyros (IRIGs,Xg,Yg,Zg), sense altitude changes, and Pulse Integrating Pendulous Accelerometers (PIPAs, Xa,Ya,Za) sense velocity changes |
| Date | |
| Source | Apollo Guidance, Navigation, and Control (GNC) Hardware Overview, https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20090016290.pdf |
| Author | NASA |
Licensing
| 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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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 23:59, 11 October 2018 | 792 × 719 (187 KB) | Pi3.124 | User created page with UploadWizard |
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