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- W2806486299 abstract "Throughout its short history, the space industry has been a subject to high levels of secrecy { initially due to concerns for national security, and more recently as a result of limitations imposed by commercial intellectual property. Fundamen- tal to a successful rocket launch, a comprehensive understanding of thrust vector control and guidance techniques are required to enable e ective rst stage system design. This shortfall in the technical literature is tackled through investigation of existing methodologies, with each selected algorithm derived from rst principles and simulated using the aerospace software package, CADAC++ [1]. The mod- elling campaign was tailored to meet the requirements of a conceptual three-stage rocket-scramjet-rocket system [2], however the fully characterised generic Small Launch Vehicle model [3] was used for simulation purposes. Results are presented demonstrating the performance of a multiple-booster thrust vector control model. Guidance simulation attempts were unsuccessful, however an analysis of the null result is presented, accompanied by recommendations for an improved simulation architecture. Fundamentally, this work culminates the body of knowledge required for the design of a rst-stage guidance module based on multiple-booster thrust vector control." @default.
- W2806486299 created "2018-06-13" @default.
- W2806486299 creator A5083092638 @default.
- W2806486299 date "2017-10-27" @default.
- W2806486299 modified "2023-10-17" @default.
- W2806486299 title "Thrust Vector Control and Guidance of a Flyback Booster during Launch" @default.
- W2806486299 hasPublicationYear "2017" @default.
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