SYSTEM FOR EVALUATION OF ACCURACY IN FORECASTING OF ARTIFICIAL EARTH SATELLITE (AES) MOTION PARAMETRES Russian patent published in 2010 - IPC B64G3/00 G01C21/00 

Abstract RU 2397927 C1

FIELD: measurement equipment.

SUBSTANCE: invention relates to procedure of trajectory measurements formation, detection of AES motion parametres using these measurements and evaluation of accuracy in forecasting of AES motion in specified range. System comprises the following blocks: initial data (1), inlet of which is inlet of system, forecasting of AES motion parametres (2), modeling of trajectory measurements (3), calculation of measured parametres values (4), detection of AES motion parametres (5), evaluation of accuracy in forecasting of AES motion parametres (6), outlet of which is the outlet of the system. Inlets and outlets of blocks are connected to each other, as indicated on circuit diagram.

EFFECT: increased accuracy and reliability in forecasting of motion parametres of wide range of AES, with provision of estimates of accuracy in forecasting of these parametres for any class of AES (low-orbit, medium-orbit and high-orbit ones).

1 dwg

Similar patents RU2397927C1

Title Year Author Number
ESTIMATION SYSTEM OF ACCURACY OF DETERMINING ARTIFICIAL EARTH SATELLITE MOVEMENT PARAMETRES 2009
  • Mikhajlova Valentina Petrovna
  • Nemtsev Vjacheslav Ivanovich
  • Sadovnikov Oleg Georgievich
RU2391265C1
ASSESSMENT SYSTEM OF INTERFERENCE IMMUNITY OF NAVIGATION CIRCUIT OF ARTIFICIAL EARTH SATELLITE (AES) 2010
  • Urlichich Jurij Matehvich
  • Kruglov Aleksandr Viktorovich
  • Sadovnikov Oleg Georgievich
  • Nemtsev Vjacheslav Ivanovich
RU2444752C1
METHOD OF DETERMINATION AND PREDICTION OF SUBJECTED TO ATMOSPHERIC BRAKING AIRCRAFT MOTION ON LOW ORBITS 2011
  • Nazarenko Andrej Ivanovich
  • Klimenko Anatolij Grigor'Evich
RU2463223C1
METHOD FOR DETERMINATION OF SPACECRAFT ORBIT 2019
  • Karavaev Dmitrij Yurevich
  • Borovikhin Pavel Aleksandrovich
  • Belyaev Mikhail Yurevich
  • Rulev Dmitrij Nikolaevich
RU2729339C1
METHOD FOR HIGH-PRECISION MEASUREMENT OF AIRCRAFT TRAJECTORY COORDINATES IN FLIGHT INVESTIGATIONS ON LONG ROUTES 2008
  • Kopylov Igor' Anatol'Evich
  • Polikarpov Valerij Georgievich
  • Padenko Viktor Mikhajlovich
  • Kharin Evgenij Grigor'Evich
  • Kopelovich Vladimir Abovich
  • Kalinin Jurij Ivanovich
  • Saparina Tat'Jana Petrovna
  • Frolkina Ljudmila Veniaminovna
  • Stepanova Svetlana Jur'Evna
RU2393430C1
METHOD FOR DETERMINING THE ORBIT OF A SPACECRAFT WITH EQUIPMENT FOR CAPTURING AN UNDERLYING SURFACE 2019
  • Karavaev Dmitrij Yurevich
  • Borovikhin Pavel Aleksandrovich
  • Belyaev Mikhail Yurevich
  • Rulev Dmitrij Nikolaevich
RU2709978C1
PROCEDURE ESTABLISHING SPACE COORDINATES OF TARGET 2002
  • Jakushin S.M.
RU2215264C1
METHOD OF SIMULATION STATISTICAL MODELING OF LOCOMOTIVE INTEGRATED NAVIGATION SYSTEM 2017
  • Maryukhnenko Viktor Sergeevich
  • Erokhin Vyacheslav Vladimirovich
RU2658509C1
METHOD FOR DETERMINATION OF SPACECRAFT ORBIT WITH EQUIPMENT FOR SHOOTING UNDERLAYING SURFACE 2019
  • Karavaev Dmitrij Yurevich
  • Borovikhin Pavel Aleksandrovich
  • Belyaev Mikhail Yurevich
  • Rulev Dmitrij Nikolaevich
RU2711834C1
ARTIFICIAL SATELLITE ONBOARD NAVIGATION SYSTEM 2013
  • Kljuchnikov Valerij Nikolaevich
RU2575302C2

RU 2 397 927 C1

Authors

Mikhajlova Valentina Petrovna

Nemtsev Vjacheslav Ivanovich

Sadovnikov Oleg Georgievich

Dates

2010-08-27Published

2009-08-17Filed