JOURNAL ARTICLE
Integration of inertial and satellite navigation systems using corrective circuits for UAV
Abstract
The scheme of integration of inertial and satellite navigation systems with corrective circuits for low-cost unmanned aerial vehicles is proposed. Based on derived mathematical model describing the errors of navigation parameters evaluation in the integrated inertial-satellite navigation system the study of system accuracy in static and dynamic operation mode has been done.
Keywords:
Inertial navigation system Satellite Computer science Inertial frame of reference Satellite navigation Inertial measurement unit Wind triangle Dead reckoning Electronic circuit Mode (computer interface) Satellite system Scheme (mathematics) Navigation system Control engineering Global Positioning System Real-time computing Engineering Aerospace engineering GNSS applications Artificial intelligence Mobile robot Electrical engineering Telecommunications Robot
Metrics
6
Cited By
0.61
FWCI (Field Weighted Citation Impact)
3
Refs
0.83
Citation Normalized Percentile
Is in top 1%
Is in top 10%
Citation History
Topics
Advanced Control and Stabilization in Aerospace Systems
Physical Sciences → Engineering → Aerospace Engineering
Advanced Research in Science and Engineering
Physical Sciences → Mathematics → Modeling and Simulation
Military Technology and Strategies
Physical Sciences → Engineering → Aerospace Engineering
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