Results 91 to 100 of about 31,323 (238)
An Improve Hybrid Calibration Scheme for Strapdown Inertial Navigation System
This paper develops an improved hybrid calibration scheme for the strapdown inertial navigation system (SINS) that combines the advantages of an optimal rotational norm calibration method and an improved system-level calibration method.
Suier Wang, Gongliu Yang, Lifen Wang
semanticscholar +1 more source
Comparison of numerical integration methods in strapdown inertial navigation algorithm
The numerical mathematical theory provides a few ways of numerical integration with different errors. It is necessary to make use of the most exact method with respect to the computing power for a majority of microprocessors, because errors are ...
V. Cviklovič +3 more
doaj +1 more source
Based on Grid Reference Frame for SINS/CNS Integrated Navigation System in the Polar Regions
As the inertial navigation system cannot meet the precision requirements of global navigation in the special geographical environment of the Polar Regions, this paper presents Strapdown Inertial Navigation System (SINS)/Celestial Navigation System (CNS ...
Song Lijun +3 more
doaj +1 more source
This paper puts forward a design method of ultra-high temperature borehole inclinometer based on fiber- optical gyroscope, and this borehole clinometer can be used for measuring the borehole trajectory and itsbending value in ultra-high temperature, and ...
Y.M. Liu, J. Wang, W.F. Ji, G.Q. Luo
doaj +1 more source
Navigation and attitude reference for autonomous satellite launch and orbital operations [PDF]
The navigation and attitude reference performance of a strapdown system are investigated for applications to autonomous satellite launch and orbital operations.
Kau, S. P.
core +1 more source
Code Optimization for Strapdown Inertial Navigation System Algorithm
Inertial navigation systems are in common use for decades due to its advantages. Since INS outputs are usually used for inputs in different control algorithms (depending on applications), INS will induce certain errors and limitations. This chapter deals with optimization of the inertial navigation algorithm against limitations due to the accuracy and ...
Todić, Ivana, Kuzmanović, Vladimir
openaire +4 more sources
Low drag attitude control for Skylab orbital lifetime extension [PDF]
In the fall of 1977 it was determined that Skylab had started to tumble and that the original orbit lifetime predictions were much too optimistic. A decision had to be made whether to accept an early uncontrolled reentry with its inherent risks or try to
Glaese, J. R., Kennel, H. F.
core +1 more source
In order to improve the precision of Strapdown Inertial Navigation System (SINS) and reduce the complexity of the traditional calibration method, a novel calibration and compensation scheme is proposed.
Jianli Li, Yanhai Ma, Chen Xiyuan
doaj +1 more source
Flight test results of the Strapdown hexad Inertial Reference Unit (SIRU). Volume 3: Appendices A-G [PDF]
Results of flight tests of the Strapdown Inertial Reference Unit (SIRU) navigation system are presented. The fault tolerant SIRU navigation system features a redundant inertial sensor unit and dual computers.
Bjorkman, W. S., Hruby, R. J.
core +1 more source
The article describes an approach to ensuring stability and controllability of unmanned aerial vehicle (UAV) with unknown aerodynamic characteristics by computer simulation of the airplane flight along a given route in the meteorological standard ...
Y. F. Yatsyna, Y. V. Gridnev
doaj +1 more source

