The work was carried out at the request of the NGO.S.A.Lavochkin, 2004
Within the framework of this work, a complex stand was developed on the basis of the EULER software complex for mathematical modeling of the stability of landing of a spacecraft (spacecraft) on Phobos.
The work was carried out jointly with FSUE TsNIIMash, 1999-2010.
The purpose of this work was to study the dynamic characteristics of processes associated with the operation of the ISS and the conduct of experiments on it, using the EULER software.
The work was carried out at the request of the GKNPTS im.M.V.Khrunichev, 2002.
The purpose of this work was to assess the unstressed separation of 2 spacecraft "Iridium" from the transitional system of the upper stage "Breeze-KM" and determine the parameters of the separation, taking into account the requirements of the interface control document.
The work was carried out jointly with the specialists of RSC Energia, 1999.
The purpose of this work was to determine the dynamic characteristics of the process of opening solar cells and the resulting loads.A characteristic feature of the design in question is the presence of a cable stabilization system, which ensures the uniformity of the process of opening the batteries.
The work was carried out jointly with the GKNPTS im.M.V.Khrunichev, 2000
Modeling of the launch of rocket and space carriers of the Angara family, taking into account the spatial dynamic interaction in the "column + retention and tracking mechanism for the ILV + launcher + ILV + control system + external environment".
The work was carried out jointly with the GKNPTS im.M.V.Khrunichev, 1999.
The purpose of the work was to determine the conditions ensuring the launchless launch of the rocket and space carrier (RKN) "Rokot".To determine the conditions of the unstressed start, a statistical simulation of the process was carried out, taking into account the probabilistic deviations of the parameters of the ILV and launch facilities, as well as external influences and initial start conditions.
Rocket and space technology
