Accession Number:

AD0269253

Title:

AN ANALYTICAL INVESTIGATION OF FLIGHT CONTROL PROBLEMS AND STATIC AND DYNAMIC RESPONSE REQUIREMENTS OF A HIGH-SPEED, LOW-ALTITUTE MISSILE

Descriptive Note:

Corporate Author:

HONEYWELL INC MINNEAPOLIS MINN

Personal Author(s):

Report Date:

1961-09-01

Pagination or Media Count:

1.0

Abstract:

The results of a study of the flight control problems of a high-speed, low-altitude missile are presented. Investigations were also made in the areas of gust analysis reactor, inlet, and control system coupling and basic vehicle stability and control. The effects of sampling frequency data rate, computation time delay, and transport lags on over-all system performance are presented. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE