A Parameter Optimization Approach to Aircraft Gust Alleviation.

Abstract

The report indicates that a knowledge of angle of attack (alpha) and/or gust perturbation angle of attack (alpha sub g) is of prime importance for a longitudinal autopilot designed to alleviate the effect of vertical gusts. However, accurate measurement of alpha and alpha sub g is extremely difficult. This research indicates that the readily measurable normal acceleration factor (n) and pitch rate (q) can be used to provide alpha and alpha sub g information indirectly. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1972
Accession Number
AD0743722

Entities

People

  • Russell Lee Clement

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Automatic Pilots
  • Control Systems
  • Flight Control Systems
  • Mathematical Analysis
  • Mathematics
  • Measurement
  • Motion
  • Numerical Analysis
  • Optimization
  • Perturbations

Fields of Study

  • Physics

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