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2013 | 19 | 85-90

Article title

Multipurpose Remotely Piloted Aircraft System Integrated Navigation System Development and Testing

Content

Title variants

Languages of publication

EN

Abstracts

EN
The paper presents development of prototype of integrated inertial-satellite navigation system that contains 3-axis accelerometers, gyros, magnetometers, barometric altimeter and GNSS (Global Navigation Satellite System) receiver. Navigation system testing procedure by means of flight at airdrome at small remotely piloted aircraft system (RPAS) is described, and data processing details with results are submitted. These results received from the data post-processing had approved the efficiency of integrated navigation system functioning in normal navigation mode, i.e. during availability of GNSS measurements. It has been shown as well that after approximately 10 s of autonomous MEMS inertial navigation system (INS) functioning accuracy of velocity and position calculation degrades significantly.

Year

Volume

19

Pages

85-90

Physical description

Contributors

  • Nacionalnyj Aviacijnyj Universytet Kyjiv
  • Nacionalnyj Aviacijnyj Universytet Kyjiv

References

Document Type

Publication order reference

Identifiers

YADDA identifier

bwmeta1.element.mhp-08cfb779-b1db-4f1f-a01b-8b1b15b4e874
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