Autonomous Guidance Reconfiguration for the Thrust Drop Fault of a Multi-satellite Launch Mission
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-6613-2_400
Reference11 articles.
1. Stender, M., Loghry, C.: Utilizing small launch vehicles for multiple small payload missions. In: 2017 IEEE Aerospace Conference, Big Sky, MT, USA (2017). https://doi.org/10.1109/AERO.2017.7943818
2. Goodman, J.: Helmut Horn and the Origin of the Saturn V Iterative Guidance Mode (IGM). AIAA SciTech Forum, Virtual Event (2021). https://doi.org/10.2514/6.2021-2020
3. Goodman, J.: Roland Jaggers and the Development of Space Shuttle Powered Explicit Guidance (PEG). AIAA SciTech Forum, Virtual Event (2021). https://doi.org/10.2514/6.2021-2021
4. Edward, M.H., Nguyen, T.X.: Space shuttle abort evolution. In: AIAA SPACE 2011 Conference & Exposition, Long Beach, California (2011). https://doi.org/10.2514/6.2011-7245
5. Tobias, M., Sauvageau, D.R., Hines, M., Geiser, N.L.: Five Segment Booster (FSB) Abort to Orbit (ATO) studies. In: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Indianapolis, Indiana (2002). https://doi.org/10.2514/6.2002-3759
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