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Flight Science and Technology

Flight Science and Technology
  • About
  • Members
  • Publications
  • Research Facilities
  • Flight Science Projects
    • Historic
    • Aircraft Handling Qualities
      • Active Control Technology for Tiltrotor
      • RHILP
      • USLOADS
      • HELIACT
    • Modelling and Simulation
    • Visual Perception
    • Advanced Configuration
  • CFD Projects

Flight Science and Technology

  • About
  • Members
  • Publications
  • Research Facilities
  • Flight Science Projects
    • Historic
    • Aircraft Handling Qualities
      • Active Control Technology for Tiltrotor
      • RHILP
      • USLOADS
      • HELIACT
    • Modelling and Simulation
    • Visual Perception
    • Advanced Configuration
  • CFD Projects
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  • Aircraft Handling Qualities > 
  • HELIACT > 
  • Research Highlights
  • HELIACT
  • Research Highlights
  • Research Publications
  • Bell 412 Modelling
  • Flight tests with the Bell 412
  • Work done by HELI-ACT member Mark Voskuijl

HELIACT - Research Highlights

Highlights of the HELIACT project include the development of a nonlinear simulation model of the Bell 412 Advanced Systems Research Aircraft and the design and flight testing of novel control laws on this aircraft. The links below provide more information.

Modelling and simulation of the Bell 412 Advanced Systems Research Aircraft

Flight tests performed with the Bell 412 ASRA

More information

  • Research Highlights
  • Research Publications
  • Bell 412 Modelling
  • Flight tests with the Bell 412
  • Work done by HELI-ACT member Mark Voskuijl
Flight Science Technology, School of Engineering, University of Liverpool
Brownlow Hill, Liverpool, L69 3GH
United Kingdom
+44 (0)151 794 4701

Call the department

+44 (0)151 794 4701