Trajectory optimization by a direct descent process
- 1 September 1968
- journal article
- research article
- Published by SAGE Publications in SIMULATION
- Vol. 11 (3) , 145-155
- https://doi.org/10.1177/003754976801100308
Abstract
The problem considered is that of trajectory optimization using step-by-step descent to minimum cost along the direction of the cost gradient with respect to the control. Using a hybrid computer, the gradient is computed di rectly as the response to nearly impulsive control perturba tions. A method is presented for computing the gradient when several terminal constraints are enforced. Examples of application of the method are presented. It is concluded that the direct gradient computation method has some significant advantages over other methods.Keywords
This publication has 2 references indexed in Scilit:
- A selected bibliography on parameter optimization methods suitable for hybrid computationSIMULATION, 1967
- Determination of Lift or Drag Programs to Minimize Re-Entry HeatingJournal of the Aerospace Sciences, 1962