Spacecraft Guidance, Navigation and Control Systems

Author(s):  
Jon H. Brown
Aviation ◽  
2010 ◽  
Vol 14 (3) ◽  
pp. 77-82 ◽  
Author(s):  
Grzegorz Kopecki ◽  
Jacek Pieniążek ◽  
Tomasz Rogalski ◽  
Pawel Rzucidło ◽  
Andrzej Tomczyk

The article presents the project of UAV control system realized at Department of Avionics and Control Systems of Rzeszów University of Technology. The project is based on earlier experiences. In the article general structure of the onboard control system is shown as well as the structure of control station. There are described in proposed control and navigation procedures as well as human factor, failure detection and system reconfiguration. Santrauka Šiame straipsnyje aprašomas bepiločiu orlaiviu kontroles sistemos projekto lgyvendinimas Ržešovo technologijos universiteto Aviadjos prietaisu ir kontroles sistemu katedroje. Projektas atliktas remiantis ankstesne patirtimi. Pateikta ne tik borto sistemu bendroji struktūra, bet ir kontroles stočiu struktūra. Darbe nagrinejamas žmogaus veiksnys, gedimu aptikimas ir sistemu rekonfigūravimas pasiūlytose kontroles ir navigacijos procedūrose.


Author(s):  
В. Б. Успенський ◽  
О. А. Татаринова ◽  
Ю. Н. Коритко

The problem of the planning of the experiment devoted to definition of the heat drifting of the angular velocity sensor is considered. The methodology for experiment program construction is proposed, with providing a number of general and specific requirements. The methodology is based on the modeling of the simplified dynamic process that describes varying internal device temperature depending on the value of the external temperature. Experimental results confirm efficiency of the developed methodology.


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