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Walter Haeussermann
Researcher at Marshall Space Flight Center
Publications - 7
Citations - 98
Walter Haeussermann is an academic researcher from Marshall Space Flight Center. The author has contributed to research in topics: Attitude control & Inertial navigation system. The author has an hindex of 6, co-authored 7 publications receiving 87 citations.
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Patent
Velocity measurement system
TL;DR: In this article, a velocity sensor for sensing the speed of a moving conductive body employing an E-shaped magnetic core having a pair of spaced Hall effect devices positioned on the end of the central core, the ends of all cores being arranged adjacent to the path of the moving conductor.
Journal ArticleDOI
Description and performance of the Saturn launch vehicle's navigation, guidance, and control system
TL;DR: Saturn launch vehicle navigation, guidance and control system, discussing optimal system design for flight path optimization as mentioned in this paper, discusses optimal trajectory optimization for a single-stage launch vehicle with a single launch vehicle.
Proceedings ArticleDOI
The pendulous integrating gyroscope accelerometer (pica) from the v-2 to trident d5, the strategic instrument of choice
TL;DR: For over 50 years, the inertial guidance industry has developed successive generations of increasingly accurate guidance navigation and control (GN&C) systems for ICBM and Submarine Launched Ballistic Missiles (SLBM) as discussed by the authors.
Proceedings ArticleDOI
Guidance and control of saturn launch vehicles.
TL;DR: Navigation, guidance and control modes and problems of Saturn launch vehicles used for Apollo missions were discussed in detail in this article, where the authors presented a detailed analysis of the Saturn launch vehicle.