Accession Number:

ADA007456

Title:

Approximate Optimum Control of the Angle of Roll in the Problem of the Re-Entry of Hypersonic Vehicles,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1975-02-04

Pagination or Media Count:

35.0

Abstract:

Subject Categories:

  • Guided Missile Trajectories, Accuracy and Ballistics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE