NASA NTRS ยท 19750009322
Techniques for trajectory optimization using a hybrid computer
Abstract
The use of a hybrid computer in the solution of trajectory optimization problems is described. The solution technique utilizes the indirect method and requires iterative computation of the initial condition vector of the co-state variables. Convergence of the iteration is assisted by feedback switching and contour modification. A simulation of the method in an on-line updating scheme is presented.
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Neely, P. L.. 1975-02-07. Techniques for trajectory optimization using a hybrid computer. https://ntrs.nasa.gov/citations/19750009322
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