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标题
作者
PRINCIPLES OF CONSTRUCTING ALGORITHMIC SUPPORT FOR AN INTELLECTUALIZED CONTROL SYSTEM FOR SPACE FLIGHT CONTROL
Soloviev S.
AUTONOMOUS GUIDANCE AND ATTITUDE CONTROL OF A SPACECRAFT IN TRACKING MODE
Somov Y., Butyrin S., Somova T.
HIGH-PRECISION SYSTEMS ADAPTATIONS TO MEASUREMENTS UNDER LOW PRESSURE
Efremkin O., Shaposhnikov S.
ECONOMICAL DIGITAL CONTROL IN EMERGENCY MODE STABILIZATION OF THE SATELLITE IN SUN-SYNCHRONOUS ORBIT
Somov Y., Butyrin S., Somova T.
DIGITAL CONTROL OF SIX GYRODINE CLUSTER AT THE SPACECRAFT INITIAL ORIENTATION
Somov Y., Butyrin S., Somov S.
SIMULATION OF THE POSITIONING PROCESS OF THE SPACECRAFT’S COMPONENTS AT THE FINAL STAGES OF ASSEMBLY
Efremkin O., Shaposhnikov S.
CONTROL OF GEOMETRIC PARAMETERS OF SLOTS FOR HIGH PRECISION INSTALLATION INSTRUMENTS
Efremkin O., Shaposhnikov S.
SELECTING THE OPTIMUM CONTROL OF A SPACECRAFT WITH THE LOW-THRUST ENGINE FULFILLING TRANSPORT TO THE INCONVERTIBLE POINT L1 OF EARTH-MOON SYSTEM
Hu Y., Starinova O.
ENSURING THE SURVIVABILITY OF SPACECRAFT CONTROL SYSTEM AT CRITICAL FAILURES OF REACTION WHEELS
Somov S., Somova T.
STABILIZATION OF A SPACECRAFT WITH ASYMMETRIC ELASTIC DESIGN IN GEOSTATIONARY ORBIT
Somov S., Somova T.
SUBSTANTIATION OF THE PARAMETERS OF BACKUP ORBITS DURING INJECTION OF THE SPACECRAFT IN CASE OF EMERGENCY CONDITIONS
Averkiev N., Vlasov S., Kulvits A., Salov V.
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