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Accession Number:
AD0269253
Title:
AN ANALYTICAL INVESTIGATION OF FLIGHT CONTROL PROBLEMS AND STATIC AND DYNAMIC RESPONSE REQUIREMENTS OF A HIGH-SPEED, LOW-ALTITUTE MISSILE
Corporate Author:
HONEYWELL INC MINNEAPOLIS MINN
Report Date:
1961-09-01
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
Pages:
0001
File Size:
0.00MB
