Add to ORKGThe processes of error development in an inertial navigation system are analysed. With this aim, the standard structures of error development were extracted in the inertial system. Error development was defined in the standard structures. Error development in the inertial navigation system is concluded according to the results obtained in the work
Dichotomizing algorithms of diagnostics and reconfiguration of the navigation system which process i...
<p>The analysis of the status of aerial photography using unmanned aerial vehicles was performed. Th...
We examine the feasibility of designing an accelerometer-based (or gyroscope-free) inertial navigati...
The processes of error development in an inertial navigation system are analysed. With this aim, the...
The article is devoted to mathematical models of errors of inertial navigation systems (INS). The ma...
INS systems are increasingly present on all vehicles and increasingly miniaturized. In this paper, w...
Content of this contribution is an issue of inertial sensors errors, specification of inertial measu...
This paper provides an overview of the primary strapdown inertial system computational elements and ...
The article considers methods of correction of navigation systems (NS) and navigation complexes (NC)...
According to the application characteristics of the K-Rb-21Ne comagnetometer, a space-stable navigat...
The operation of technical processes requires increasingly advanced supervision and fault diagnostic...
Error distribution analysis is an important assistant technology for the research of SINS(Strapdown ...
Attitude error models play an important role in analyzing the characteristics of navigation error pr...
Errors of INS output parameters lead to a positive feedback effect of errors and eventually to an ev...
Errors of INS output parameters lead to a positive feedback effect of errors and eventually to an ev...
Dichotomizing algorithms of diagnostics and reconfiguration of the navigation system which process i...
<p>The analysis of the status of aerial photography using unmanned aerial vehicles was performed. Th...
We examine the feasibility of designing an accelerometer-based (or gyroscope-free) inertial navigati...
The processes of error development in an inertial navigation system are analysed. With this aim, the...
The article is devoted to mathematical models of errors of inertial navigation systems (INS). The ma...
INS systems are increasingly present on all vehicles and increasingly miniaturized. In this paper, w...
Content of this contribution is an issue of inertial sensors errors, specification of inertial measu...
This paper provides an overview of the primary strapdown inertial system computational elements and ...
The article considers methods of correction of navigation systems (NS) and navigation complexes (NC)...
According to the application characteristics of the K-Rb-21Ne comagnetometer, a space-stable navigat...
The operation of technical processes requires increasingly advanced supervision and fault diagnostic...
Error distribution analysis is an important assistant technology for the research of SINS(Strapdown ...
Attitude error models play an important role in analyzing the characteristics of navigation error pr...
Errors of INS output parameters lead to a positive feedback effect of errors and eventually to an ev...
Errors of INS output parameters lead to a positive feedback effect of errors and eventually to an ev...
Dichotomizing algorithms of diagnostics and reconfiguration of the navigation system which process i...
<p>The analysis of the status of aerial photography using unmanned aerial vehicles was performed. Th...
We examine the feasibility of designing an accelerometer-based (or gyroscope-free) inertial navigati...