Integrated solution to the problem of estimation and identification of a state vector of the gimballess navigation system of a reentry spacecraft

Author： Pogorelov V.

Publisher： MAIK Nauka/Interperiodica

ISSN： 0010-9525

Source： Cosmic Research, Vol.44, Iss.3, 2006-05, pp. : 268-275

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

Determination of the width of a corridor of re-entry into the atmosphere for the problem of launching a spacecraft into a circumplanetary orbit after braking in the atmosphere

By Yaroshevskii V.

Cosmic Research, Vol. 44, Iss. 3, 2006-05 ,pp. : 236-244

MAIK Nauka/Interperiodica

Access to resources Recommend Favorite

Application of information criteria to control the structurally uncertain navigation system of a reusable spacecraft

By Pogorelov V.

Cosmic Research, Vol. 47, Iss. 1, 2009-02 ,pp. : 44-52

MAIK Nauka/Interperiodica

Access to resources Recommend Favorite

An integrated aircraft navigation system with optical horizon sensor

By Rahmouni Mohamed

Aviation, Vol. 16, Iss. 4, 2012-12 ,pp. : 109-114

Taylor & Francis Ltd

Access to resources Recommend Favorite

Estimation of the Probability of Radiation Failures and Single Particle Upsets of Integrated Microcircuits onboard the Fobos-Grunt Spacecraft

By Kuznetsov N. Popov V. Khamidullina N.

Cosmic Research, Vol. 43, Iss. 3, 2005-05 ,pp. : 225-227

MAIK Nauka/Interperiodica

Access to resources Recommend Favorite

Comprehensive analysis and estimation system on thermal environment, heat protection and thermal structure of spacecraft

By Guoliang M. Guiqing J.

Acta Astronautica, Vol. 54, Iss. 5, 2004-03 ,pp. : 347-356

Elsevier

Access to resources Recommend Favorite