AUTONOMOUS NAVIGATION SYSTEM OF SMALL SPACECRAFT
Annotation
An approach to the problem of maintenance of stable functioning of small spacecraft is considered. The essence of the approach consists in integration of autonomous navigation system into the small spacecraft onboard control complex to allow for measurement of the primary navigation parameters just on board. An algorithm of joint information processing with the use of the least squares method is proposed.
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Articles in current issue
- ANALYSIS OF CURRENT STATE AND PROSPECT FOR THE DEVELOPMENT OF BOKZ STAR TRACKERS FAMILY
- AUTONOMOUS NAVIGATION SYSTEM OF SMALL SPACECRAFT
- ALGORITHM OF DYNAMICAL ESTIMATION OF OBJECT ORIENTATION PARAMETERS FROM SATELLITE MEASUREMENTS
- AMBIGUITY RESOLUTION OF PHASE MEASUREMENTS AND SELECTION OF CARRIER FREQUENCIES IN SATELLITE NAVIGATING SYSTEM
- ESTIMATION OF ACCURACY CHARACTERISTICS OF CARRIER ROCKET CONTROL SYSTEM BY RESULTS OF LAUNCHES UNDER VARIOUS CONDITIONS
- ADAPTIVE CONTROL OVER LATERAL MOVEMENT OF AIRCRAFT IN THE LANDING MODE
- DISPLACEMENT CONTROL IN OPTICAL-ELECTRONIC SYSTEMS WITH OPTICAL EQUISIGNAL ZONE
- DETERMINATION OF OPTICAL COMPONENTS BASIC PARAMETERS OF OPTICAL SYSTEM WITH VARIABLE MAGNIFICATION
- PROBABILISTIC ANALYSIS OF DATA GATHERING AND PROCESSING CENTER OPERATION
- CREATION OF ANALYTIC SIGNAL WITH A KNOWN ELEMENTARY PHASE
- EFFECTIVE METHOD OF ACCELERATED LIFE TEST OF FRICTION ASSEMBLY
- PERMANENT MAGNET SYNCHRONOUS MOTOR TORQUE
- MODEL OF VISUAL MEASUREMENTS
- FIVE-LAYER QUARTER-WAVE ANTIREFLECTION COATING ON THE BASE OF THREE FILM-FORMING MATERIALS
- APPLICATION OF MATLAB SOFTWARE IN EDUCATIONAL PROCESS FOR MODELING OF MECHATRONIC SYSTEMS