![Scientific and technical journal «Priborostroenie»](/images/mag-pr.png)
METHOD OF SELECTING THE PROGRAM OF NANOSATELLITES GROUP SEPARATION FROM THE SPACE PLATFORM
![Scientific and technical journal «Priborostroenie»](/images/mag-pr.png)
Annotation
A method of selection of the program of nanosatellites separation from an undirected space platform at the stage of a flight task formulation is proposed. The method is based on statistical researches and provides a predetermined character relative motion of nanosatellites. The choice of the nanosatellite separation parameters is based on the application of a criterion that describes the maximum distance between each pair of nanosatellites, with the exception of the possibility of their dangerous approach both with each other and with the platform from which they are separated. As a result, the separation parameters are selected, for which the maximum value of the distance between the nanosatellite is minimal and thus the flight safety is ensured. The method is demonstrated in details by the example of nanosatellites group separation from the orbital stage of "Soyuz" carrier rocket.
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Articles in current issue
- LIDAR SOUNDING OF THE UPPER LAYERS OF THE ATMOSPHERE AND THE F-LAYER OF THE IONOSPHERE WITH THE USE OF NANOSATELLITES GROUPS
- COMPLEX OF SMALL-SIZED APPLIANCES FOR SPACE WEATHER RESEARCH
- CUBESAT ONBOARD CONTROL SYSTEM ON THE BASE OF „SYSTEM-ON-CHIP“ TECHNOLOGY
- MODIFIED ALGORITHM FOR ESTIMATING THE UNIAXIAL ORIENTATION OF NANOSATELLITE BY GEOMETRIC VISIBILITY OF NAVIGATION SPACECRAFTS
- INCREASING THE TARGET EFFICIENCY OF INFORMATION SUPPORT NANOSATELLITES
- NEW CUBESAT ARCHITECTURE WITHOUT ONBOARD CABLE NETWORK
- MODELING OF THERMAL MODE OF MICROSATELLITE OPTICAL-ELECTRONIC TELESCOPIC COMPLEX
- APPLICATION OF THE GNSS NAVIGATION APPARATUS ON BOARD A NANOSATELLITE
- UNIVERSAL PAYLOAD PLATFORM FOR SMALL SATELLITES OF THE CUBESAT STANDARD
- RESONANT MOTION OF NANOSATELLITE OF CUBESAT STANDARD IN LOW CIRCULAR ORBITS