Development of a Continuous Performance Measure for Manual Control.

Abstract

The performance measurement concept typically applied to manual control systems employs a summary measure which provides a numerical score to represent performance of the total control problem. While summary measures are necessary for evaluating total performance they do not reveal information about control actions that occur during the control problem. If performance can be measured and evaluated continuously throughout the control problem each control action can be evaluated rapidly and thus individually. Also if the continuous measurement and evaluation can be related to the summary measure, each control action can be evaluated as an entity, as well as, part of the total control problem. The desired continuous performance measure (CPM) provides a continuous indication of the correct motion of the aircraft at each point in a mission segment and what is also important, an indication of the significance of any motion errors with respect to the summary measure performance selected. This application of the continuous performance measure is termed the 'Mission Model' since the model can provide both reference aircraft motion and an evaluation of the flight control errors. The objective of the research reported here is to evaluate the feasibility of continuous performance measures for aircraft systems, and the development of the necessary computational tools.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1977
Accession Number
ADA041676

Entities

People

  • E. M. Connelly
  • G. P. Chubb
  • R. M. Zeskind

Tags

Communities of Interest

  • Air Platforms
  • Human Systems
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Capillary Electrophoresis
  • Computational Science
  • Computer Programming
  • Computer Programs
  • Computer Simulations
  • Computers
  • Control Systems
  • Differential Equations
  • Equations Of State
  • Human Factors Engineering
  • Mathematical Models
  • Military Aircraft
  • Navigation
  • Systems Engineering
  • Time Intervals

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Aviation Science / Aeronautics.
  • Theoretical Analysis.