Dynamics and control of launch vehicles  

Course content covers the fundamentals of launch vehicle flight mechanics, including the optimal planning of the ascent trajectory of a (possibly reusable) launch vehicle from the launch base to payload insertion into orbit, and the analysis of stability and control of the vehicle in atmospheric flight. Key factors affecting launch vehicle performance, such as mission requirements, atmospheric conditions, and launch-site location, will also be explained to provide students with a comprehensive understanding of the context in which launch vehicles operate. The course give emphasis on the ability to apply the knowledge learned to solve numerical problems typical of launch vehicle flight mechanics, such as trajectory planning and control of a large flexible booster.
Presential
English
Dynamics and control of launch vehicles
English

Funded by the European Union. Views and opinions expressed are however those of the author(s) only and do not necessarily reflect those of the European Union or HaDEA. Neither the European Union nor the granting authority can be held responsible for them. The statements made herein do not necessarily have the consent or agreement of the ASTRAIOS Consortium. These represent the opinion and findings of the author(s).