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

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.

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Document Details

Document Type
Technical Report
Publication Date
Feb 24, 1961
Accession Number
AD0271570

Entities

People

  • C. B. Exby
  • J. R. Gray
  • J. W. Harrison

Organizations

  • Honeywell International, Inc.

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Sensors
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aircrafts
  • Checkout Equipment
  • Checkout Procedures
  • Circuit Analysis
  • Control Systems Engineering
  • Electron Tubes
  • Flight Control Systems
  • Life Tests
  • Measurement
  • Reliability
  • Switching
  • Test And Evaluation
  • Test Equipment
  • Test Facilities
  • Test Methods
  • Transducers

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Software Engineering