Optimal shuttle trajectory - Vehicle design using parameter optimization
I. L. Johnson, James L. Kamm
Abstract
I. L. Johnson, James L. Kamm
Abstract
Space shuttle optimal design problem, applying accelerated gradient parameter optimization technique
OpenAlex reports 8 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
Space shuttle optimal design problem, applying accelerated gradient parameter optimization technique
Key concepts: Trajectory optimization, Trajectory, Space Shuttle, Computer science, Mathematical optimization, Control theory (sociology), Engineering, Optimal control