Accession Number:

AD0271570

Title:

ADVANCED FLIGHT VEHICLE SELF-ADAPTIVE FLIGHT CONTROL SYSTEM. PART 3. SUPPORT EQUIPMENT STUDY

Descriptive Note:

Corporate Author:

HONEYWELL INC MINNEAPOLIS MN

Report Date:

1961-02-24

Pagination or Media Count:

77.0

Abstract:

Results are presented of the design study to develop the ground support equipment for the MH-96 Adaptive Flight Control System to be tested in the X-15 aircraft. Design solutions are presented which reflect the problem areas that became apparent as the designs of the ground support equipment progressed. Since the final flight control system design changes have not yet been made, the GSE solutions have also not been finalized. However, this report presents a summary of the design practices being followed in the development of the ground support equipment for the MH-96 Adaptive Flight Control System.

Subject Categories:

  • Research and Experimental Aircraft
  • Flight Control and Instrumentation
  • Terminal Flight Facilities

Distribution Statement:

APPROVED FOR PUBLIC RELEASE