An Automated Method to Compute Orbital Re-Entry Trajectories with Heating Constraints by Curtis Zimmerman

An Automated Method to Compute Orbital Re-Entry Trajectories with Heating Constraints

Curtis Zimmerman

28 pages missing pub info (editions)

nonfiction politics
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Description

Determining how to properly manipulate the controls of a re-entering re-usable launch vehicle (RLV) so that it is able to safely return to Earth and land involves the solution of a two-point boundary value problem (TPBVP). This problem, which can ...

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