Abstract
The safety and reliability of the rocket will be greatly improved via trajectory re-planning design in case of propulsion system failure, which is a key technology for design and development of new generation launch vehicles. This section takes the two-stage launch vehicle as an example, and different trajectory re-planning schemes are designed according to the characteristics of launch vehicle in different flight stages, to adapt to the trajectory planning and command reconstruction under different fault conditions during flight.
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Li, X., Xu, F., Xu, G. (2023). Multistage Rocket Trajectory Re-planning. In: Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle. Navigation: Science and Technology, vol 12. Springer, Singapore. https://doi.org/10.1007/978-981-19-4637-0_7
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DOI: https://doi.org/10.1007/978-981-19-4637-0_7
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Publisher Name: Springer, Singapore
Print ISBN: 978-981-19-4636-3
Online ISBN: 978-981-19-4637-0
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