Results 91 to 100 of about 32,114 (240)
Comparison of numerical integration methods in strapdown inertial navigation algorithm
Research in Agricultural Engineering, 2011 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
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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.
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Обзор существующих автономных и интегрированных навигационных систем для армейских машин [PDF]
, 2009 В статті наведені основні характеристики навігаційних систем армійських машин ведучих країн світу. Розглянуті основні типи датчикової апаратури, що використовуються в безплатформених інерціальних навігаційних системах.In report the characteristics of the
Беляев, С. Н. +2 more
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Code Optimization for Strapdown Inertial Navigation System Algorithm
, 2018 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.
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Abstract and Applied Analysis, 2013 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
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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.
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Весці Нацыянальнай акадэміі навук Беларусі: Серыя фізіка-тэхнічных навук, 2018 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
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SIRU development. Volume 1: System development [PDF]
A complete description of the development and initial evaluation of the Strapdown Inertial Reference Unit (SIRU) system is reported. System development documents the system mechanization with the analytic formulation for fault detection and isolation ...
Cooper, R. J., Gilmore, J. P.
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Optimization of a New High Rotary Missile-Borne Stabilization Platform
Sensors, 2019 The passive semi-strapdown roll stabilized platform is an inertial platform, which can isolate the rolling of a projectile body by a special mechanical device.
Xiaokai Wei +6 more
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