Chapter 5. Modelling Helicopter Flight Dynamics: Stability Under Constraint and Response Analysis

  1. Gareth D. Padfield BSc, PhD, C Eng, FRAeS

Published Online: 15 APR 2008

DOI: 10.1002/9780470691847.ch5

Helicopter Flight Dynamics: The Theory and Application of Flying Qualities and Simulation Modelling, Second Edition

Helicopter Flight Dynamics: The Theory and Application of Flying Qualities and Simulation Modelling, Second Edition

How to Cite

Padfield, G. D. (2007) Modelling Helicopter Flight Dynamics: Stability Under Constraint and Response Analysis, in Helicopter Flight Dynamics: The Theory and Application of Flying Qualities and Simulation Modelling, Second Edition, Blackwell Publishing Ltd, Oxford, UK. doi: 10.1002/9780470691847.ch5

Publication History

  1. Published Online: 15 APR 2008
  2. Published Print: 1 JAN 2007

ISBN Information

Print ISBN: 9781405118170

Online ISBN: 9780470691847

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Keywords:

  • attitude constraint;
  • flight-path constraint;
  • collective control inputs;
  • cyclic pitch control inputs;
  • atmospheric disturbances

Summary

This chapter contains section titled:

  • Introduction and Scope

  • Stability Under Constraint

  • Analysis of Response to Controls

  • Response to Atmospheric Disturbances