Simulation of coupled helicopter-slung load-pilot dynamics

Jacob Enciu, Aviv Rosen

Research output: Contribution to journalArticlepeer-review

5 Scopus citations

Abstract

A nonlinear simulation of a helicopter carrying a fin-stabilized underslung load was developed. Simulation predictions were validated using comparisons to flight-test results. A human pilot model was incorporated in the simulation to study the dynamics and stability of the helicopter-slung load-pilot system. Simulation results and their subsequent analysis show that the underslung load is stabilized by the helicopter. These results confirm observations from flight tests regarding the critical role of the piloting technique in determining the stability of the system. Pilot attempts to counteract load lateral oscillations by applying lateral stick commands cause the system to become unstable and result in pilot-induced oscillations. Freezing the lateral stick causes load oscillations to completely decay or damp down to very low residual amplitudes. The effect of piloting technique diminishes at high airspeeds due to the increase in load stability.

Original languageEnglish (US)
Article number012007
JournalJournal of the American Helicopter Society
Volume62
Issue number1
DOIs
StatePublished - Jan 2017

All Science Journal Classification (ASJC) codes

  • Materials Science(all)
  • Aerospace Engineering
  • Mechanics of Materials
  • Mechanical Engineering

Fingerprint Dive into the research topics of 'Simulation of coupled helicopter-slung load-pilot dynamics'. Together they form a unique fingerprint.

Cite this