This paper focuses on the different powered descent and landing studies in atmosphere performed to formulate the landing guidance problem for the CALLISTO vehicle, a technological demonstrator jointly developed by DLR, JAXA, and CNES. By formulating and solving different optimal control problems we critically compare the results to come up with a satisfactory trade-off that balances performance and safety concerns.
Sagliano, M., Heidecker, A., Fari, S., Hernandez, J.M., Schlotterer, M., Woicke, S., et al. (2024). Powered Atmospheric Landing Guidance for Reusable Rockets: the CALLISTO studies. American Institute of Aeronautics and Astronautics Inc, AIAA [10.2514/6.2024-1761].
Powered Atmospheric Landing Guidance for Reusable Rockets: the CALLISTO studies
Sagliano M.
;
2024
Abstract
This paper focuses on the different powered descent and landing studies in atmosphere performed to formulate the landing guidance problem for the CALLISTO vehicle, a technological demonstrator jointly developed by DLR, JAXA, and CNES. By formulating and solving different optimal control problems we critically compare the results to come up with a satisfactory trade-off that balances performance and safety concerns.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
