Spacecraft Dynamics and Control

On the construction of an adaptable system of mutual measurements for autonomous rendezvous of spacecrafts with non-cooperative space objects

Development of a high-speed software package for calculating the trajectory of launching a spacecraft into a geostationary orbit using the gravitational field of the moon with visualization of calculations

Reliability increment of onboard control complexes by means of lockstepped hardware voting majority frames construction at hardware synchronization of single-chip microcontrollers

Investigation of the possibility of ballistic factor chage predicting on the basis of outer-trajectory measurements with the use of stable atmosphere parameters for calculations