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ARTIS UAS

RI-036
Flight Test Bed
Infrastructure
DLR
Description

2 Research Helicopters plus Ground Control Station

Main technical characteristics

Type of flight vehicle Unmanned Helicopter
Main features Research testbed, modular payload, intermeshing rotor, turbine engine
Control system Proprietary, start, waypoint, landing
Maximum altitude 3000 m
Measurement instruments5 Internal states, flight test instrumentation, imaging and laser scanner sensors, research grade IMU
Comment F / T

Contact Information
Gordon Strickert, E-mail: Gordon.Stri...
Brunswick (Germany)
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  • About
    • About EREA
    • Members
    • Organisation
    • EREA in Flightpath 2050
    • Events
    • Position Papers
    • Publications
    • Vacancies
    • Contact us
  • Capabilities
  • Technology Infrastructures
    • TRIG
    • Catalogue
  • European Cooperation
  • Future Sky
  • News
  • Intranet
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