FIELD: aircraft engineering.
SUBSTANCE: spacecraft is placed to orbit. Spacecraft onboard hardware comprises navigation devices of global navigation satellite system consumer and hardware for measurement of frequency of signal transmitted by observed spacecraft. During spacecraft orbital flight orbit parameters are defined with the help of consumer navigation hardware. Observed spacecraft signal frequency measurement program is developed to measure the frequency of said signal. Measured signal frequency is used as the navigation parameter of observed spacecraft orbit. Measured navigation parameters are accumulated and measurement results are processed. Observed spacecraft orbit is defined from measured signal frequency magnitudes and spacecraft orbit parameters.
EFFECT: accelerated measurements required for orbit determination.
1 dwg, 2 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR EPHEMERAL PROVISIONING OF PROCESS FOR CONTROLLING GLOBAL NAVIGATION SATELLITE SYSTEM SPACECRAFT | 2011 |
|
RU2477836C1 |
| METHOD FOR EPHEMERAL CONTROL OF SPACECRAFT GLOBAL NAVIGATION SATELLITE SYSTEM | 2009 |
|
RU2390730C1 |
| METHOD FOR BUILDING OF ORBIT-BASED FUNCTIONAL ADDITION TO GLOBAL NAVIGATION SYSTEM | 2008 |
|
RU2367910C1 |
| METHOD OF MONITORING CONTINUITY OF NAVIGATION FIELD OF GLOBAL NAVIGATION SATELLITE SYSTEM | 2011 |
|
RU2477835C1 |
| METHOD FOR NAVIGATION CONTROL OF SPACECRAFT INJECTION ORBITS AND A SYSTEM FOR ITS IMPLEMENTATION | 2021 |
|
RU2759173C1 |
| METHOD FOR DETECTION OF ANGULAR ORIENTATION OF SPACECRAFT BY SIGNAL OF RADIO NAVIGATION ORIENTATOR | 2008 |
|
RU2367909C1 |
| METHOD FOR REAL-TIME MONITORING OF INTEGRITY OF NAVIGATION FIELD OF GLOBAL NAVIGATION SATELLITE SYSTEM | 2014 |
|
RU2584091C1 |
| METHOD OF DEFINING SPACECRAFT ORBIT | 2012 |
|
RU2509041C1 |
| METHOD OF DETERMINING POSITION OF NAVIGATION INFORMATION USER OBJECTS AND DEVICE FOR REALISING SAID METHOD | 2009 |
|
RU2402786C1 |
| METHOD FOR ANGULAR ORIENTATION OF OBJECT | 2015 |
|
RU2580827C1 |
