Accession Number:

ADA007400

Title:

Optimum Control of Flight Vehicle Under the Conditions of Uncertainty,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1975-02-13

Pagination or Media Count:

26.0

Abstract:

Subject Categories:

  • Guided Missile Trajectories, Accuracy and Ballistics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE