Attitude and heading reference system with acceleration compensation

Author： Hemerly Elder M.   Maciel Benedito C.O.   Milhan Anderson de P.   Schad Valter R.  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.84, Iss.2, 2012-03, pp. : 87-93

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Testing of the attitude and heading reference system

By Tomczyk Andrzej  

Aircraft Engineering, Vol. 74, Iss. 2, 2002-04 ,pp. : 154-160

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Software algorithms in air data attitude heading reference systems

By Greene Michael E.   Trent Victor  

Aircraft Engineering, Vol. 75, Iss. 5, 2003-09 ,pp. : 470-476

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Operation for the combined energy and attitude control system

By Varatharajoo Renuganth  

Aircraft Engineering, Vol. 78, Iss. 6, 2006-11 ,pp. : 495-501

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Design and analysis of nano momentum wheel for picosatellite attitude control system

By Jayaram Sanjay  

Aircraft Engineering, Vol. 81, Iss. 5, 2009-09 ,pp. : 424-431

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Attitude control system of the first Russian nanosatellite TNS-0 no. 1

By Karpenko S.   Kupriyanova N.   Ovchinnikov M.   Penkov V.   Selivanov A.   Khromov O.  

Cosmic Research, Vol. 48, Iss. 6, 2010-12 ,pp. : 517-525

MAIK Nauka/Interperiodica

Access to resources Recommend Favorite