Add to ORKGThe paper considers dynamic test table system for navigation sensors testing and verification. The problem of test table confidence margin is considered taking into account different sources of errors. Estimation of frequency characteristics of sensors is shown by special test table criteria.The paper describes inertial navigation system experiment on dynamic test table in order to compensate navigation system parameters
Content of this contribution is an issue of inertial sensors errors, specification of inertial measu...
This paper summarizes some of the joint research efforts of University of Minnesota, University of S...
Abstract. In this article the methods of increase the efficiency of the compensation of indignations...
Ukraine Section SP/AES Joint ChapterThe paper shows how dynamic hardware-in-the-loop ground test s...
Unmanned aerial vehicle flight simulation bench for visual navigation system. Visual nav...
Designed system for microelectromechanical sensors testing before use them in the unmanned aerial...
The dominant navigation system for small civilian UAVs today is based on integration of inertial nav...
This paper presents extensions and practical realization of a previously proposed novel approach to ...
The operation of technical processes requires increasingly advanced supervision and fault diagnostic...
The development of informatics and sensor techniques has extended the possibilities of flight parame...
This thesis details the effective integration of global navigation satellite systems (GNSS) with an ...
The paper presents development of prototype of integrated inertial-satellite navigation system that ...
The unmanned aerial vehicle (UAV) recovery method, especially for an emergency situation, is an impo...
The Vehicle Dynamic Model (VDM) based navigation of fixed-wing drones determines the airborne trajec...
To overcome the rapid and unbounded error growth of low-cost Inertial Navigation Systems (INS), airc...
Content of this contribution is an issue of inertial sensors errors, specification of inertial measu...
This paper summarizes some of the joint research efforts of University of Minnesota, University of S...
Abstract. In this article the methods of increase the efficiency of the compensation of indignations...
Ukraine Section SP/AES Joint ChapterThe paper shows how dynamic hardware-in-the-loop ground test s...
Unmanned aerial vehicle flight simulation bench for visual navigation system. Visual nav...
Designed system for microelectromechanical sensors testing before use them in the unmanned aerial...
The dominant navigation system for small civilian UAVs today is based on integration of inertial nav...
This paper presents extensions and practical realization of a previously proposed novel approach to ...
The operation of technical processes requires increasingly advanced supervision and fault diagnostic...
The development of informatics and sensor techniques has extended the possibilities of flight parame...
This thesis details the effective integration of global navigation satellite systems (GNSS) with an ...
The paper presents development of prototype of integrated inertial-satellite navigation system that ...
The unmanned aerial vehicle (UAV) recovery method, especially for an emergency situation, is an impo...
The Vehicle Dynamic Model (VDM) based navigation of fixed-wing drones determines the airborne trajec...
To overcome the rapid and unbounded error growth of low-cost Inertial Navigation Systems (INS), airc...
Content of this contribution is an issue of inertial sensors errors, specification of inertial measu...
This paper summarizes some of the joint research efforts of University of Minnesota, University of S...
Abstract. In this article the methods of increase the efficiency of the compensation of indignations...