Accession Number:

AD0271846

Title:

OPTIMUM PROGRAMMING OF THE THRUST OF THE POWER UNIT WHEN THE FLIGHT TRAJECTORY IS GIVEN

Personal Author(s):

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1962-02-05

Abstract:

The problem is analyzed of determining the optimum programming of the power units thrust, which will guarantee reaching a certain integral characteristic of motion for example, range of flight, initial weight, and time consumed in reaching goal of extremal value at a given trajectory. Author

Pages:

0013

Descriptors:

Identifiers:

File Size:

0.00MB

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