An Investigation of Displayed Ground Referenced Position, Velocity, and Acceleration for Precision Hover

Abstract

This report presents a man-machine simulation investigation of displayed ground referenced acceleration, velocity, and position for a manual precision hover task. The study determined the appropriate display gains for the above parameters as a function of three different control systems: the Automatic Stabilization Equipment (ASE), the Stability Augmentation System (SAS) and the Hover Augmentation System (HAS).

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1975
Accession Number
ADA012813

Entities

People

  • C. M. Tsoubanos

Organizations

  • United States Army Communications-Electronics Command

Tags

Communities of Interest

  • Air Platforms
  • Sensors

DTIC Thesaurus Topics

  • Aircrafts
  • Altitude
  • Automatic
  • Closed Loop Systems
  • Control Systems
  • Data Analysis
  • Digital Data
  • Flight
  • Frequency
  • Military Aircraft
  • Radar Altimeters
  • Research Aircraft
  • Simulations
  • Simulators
  • Training
  • Transfer Functions
  • Workload

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Computer Science.