FIELD: aviation.
SUBSTANCE: system includes one or more spacecraft, positioned in the orbit of the Earth at a constant distance from it, and land tools of control, reception of information from the spacecraft and processing the received information. Spacecrafts carry out constant surveillance of the part of outer space between the Sun and the Earth, which is due to Sun exposure is not available for observation from the Earth and near-earth orbits. This space represents a cone with its apex on Earth, with an axis directed towards the Sun, and the angle at the top equal to the Sun angle of optical sensors placed on the Earth and on near-earth orbits. Land control and navigation center (LCNC) generates and transmits control commands, outer space scanning software and times of radiovisibility with ground equipment for information reception on spacecraft. Spacecraft (spacecrafts) daily on intervals of radiovisibility time of ground equipment transmits on it the information received both in real time and saved in observations outside of radiovisibility intervals. Ground information processing center, which is part of the LCNC, carries out the processing of information received, and produces the final information about detected celestial bodies. In case of detection of potentially dangerous celestial bodies LCNC produces through block of connection with subscribers of the system in a consistent format this information to organs of government, EMERCOM and other organizations belonging to outside party of proposed space system. This space system can also be used to conduct astronomical research.
EFFECT: enhancing functional capacity.
3 cl 7 dwg
Title | Year | Author | Number |
---|---|---|---|
SPACE SYSTEM FOR VIEWING CELESTIAL SPHERE FOR OBSERVING CELESTIAL OBJECTS AND DETECTING CELESTIAL BODIES - ASTEROIDS AND COMETS - HAZARDOUS FOR EARTH | 2015 |
|
RU2610066C1 |
METHOD OF COELOSPHERE COVERAGE FROM SPACE CRAFT FOR SURVEILLANCE OF CELESTIAL BODIES AND COELOSPHERE COVERAGE SPACE SYSTEM FOR SURVEILLANCE OF CELESTIAL BODIES AND DETECTION OF SOLAR SYSTEM BODIES TO THIS END | 2012 |
|
RU2517800C1 |
METHOD OF SCANNING SPACE BETWEEN THE SUN AND THE EARTH, NOT AVAILABLE FOR OBSERVATION OF OPTICAL DEVICES LOCATED ON GROUND AND ON EARTH ORBITS DUE TO THEIR ILLUMINATION OF THE SUN WITH SPACECRAFT ARRANGED AT THE ORBIT OF THE EARTH AT A CONSTANT DISTANCE FROM THE EARTH | 2015 |
|
RU2597028C1 |
METHOD OF THE CELESTIAL SPHERE SPACE SURVEILLANCE SYSTEM FOR APPROACHING FROM THE SUN CELESTIAL BODIES DETECTION AND THREATENING COLLISION WITH THE EARTH | 2017 |
|
RU2660090C1 |
APPROACHING EARTH FROM THE DAYTIME SKY DANGEROUS CELESTIAL BODIES DETECTION METHOD AND THE SODA-2 SPACE SYSTEM FOR ITS IMPLEMENTATION | 2017 |
|
RU2675205C1 |
MONITORING OF ASTEROID-COMET DANGER | 2014 |
|
RU2573509C1 |
METHOD FOR OBSERVING ASTEROIDS ACROSS THE ENTIRE CELESTIAL SPHERE | 2020 |
|
RU2753200C1 |
METHOD OF PRESENTATION OF LIGHT IMAGES OVER CELESTIAL SPHERE | 1992 |
|
RU2047911C1 |
INTERNATIONAL GLOBAL MONITORING AEROSPACE SYSTEM (IGMAS) | 2010 |
|
RU2465729C2 |
METHOD OF THE GEOSTATIONARY REGION SURVEY FOR THE SPACE DEBRIS ELEMENTS AND OTHER OBJECTS OBSERVATION FROM SPACE CRAFT ON THE SEMI-DIURNAL HIGH-ELLIPTIC ORBIT | 2017 |
|
RU2659379C1 |
Authors
Dates
2017-06-06—Published
2015-12-03—Filed