Trajectory optimization of the Brazilian multistage launch vehicle VLM-1
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics
Link
https://link.springer.com/content/pdf/10.1007/s40430-023-04490-6.pdf
Reference38 articles.
1. Rao AV (2010) A survey of numerical methods for optimal control. Adv Astronaut Sci 135:497–528
2. Betts JT (1998) Survey of numerical methods for trajectory optimization. J Guid Control Dyn 21:193–207. https://doi.org/10.2514/2.4231
3. von Stryk O, Bulirsch R (1992) Direct and indirect methods for trajectory optimization. Ann Oper Res 37:357–373. https://doi.org/10.1007/BF02071065
4. Shrivastava SK, Reddy MN (1976) Determination of optimal trajectory under design constraints for a satellite launch vehicle. Acta Astronaut 3:333–347. https://doi.org/10.1016/0094-5765(76)90140-5
5. Adimurthy V (1987) Launch vehicle trajectory optimization. Acta Astronaut 15:845–850. https://doi.org/10.1016/0094-5765(87)90039-7
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