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Entry trajectory optimization for hypersonic vehicles has been formulated as constrained optimal control problems, which are difficult to solve because of the existing high nonlinearity and nonconv... Click to show full abstract
Entry trajectory optimization for hypersonic vehicles has been formulated as constrained optimal control problems, which are difficult to solve because of the existing high nonlinearity and nonconv...
Keywords:
entry trajectory;
improved sequential;
trajectory optimization
Journal Title: Journal of Spacecraft and Rockets
Year Published: 2020
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Journal Title: Journal of Spacecraft and Rockets
Year Published: 2020
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!