FIELD: aircraft instrumentation engineering; systems forming relative coordinates for group actions of flying vehicles. SUBSTANCE: information system includes satellite coordinate sensor, inertial coordinate sensor, data receiving and transmitting unit, first to "n" correction units; optimal information processing unit provides for correction from satellite coordinate sensor at "n" probable combinations of satellite in area of actions; in this case, constant component is absent in relative coordinate error at interaction with system of other flying vehicle. Many estimates of relative coordinates are averaged in optimal information processing unit introduced in system additionally; relative coordinates are formed in this unit. EFFECT: enhanced efficiency. 2 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
INFORMATION LANDING SYSTEM | 1992 |
|
RU2023984C1 |
COMPLEX NAVIGATION SYSTEM | 1992 |
|
RU2023983C1 |
COMPLEX COMPASS SYSTEM | 1996 |
|
RU2098322C1 |
COMPLEX SYSTEM OF NAVIGATIONAL SUPPORT OF APPROACH | 1992 |
|
RU2042923C1 |
INFORMATION SYSTEM FOR FORMATION OF ABSOLUTE ALTITUDE | 1994 |
|
RU2085851C1 |
SYSTEM FOR CONTROL OF FLIGHT ALTITUDE AT LANDING | 1996 |
|
RU2102281C1 |
COMPLEX INERTIAL SYSTEM | 1996 |
|
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COMPLEX SYSTEM TO FORM AIR PARAMETERS | 1998 |
|
RU2146805C1 |
COMPLEX NAVIGATIONAL SYSTEM | 2000 |
|
RU2168704C1 |
COMPLEX NAVIGATION SYSTEM | 1998 |
|
RU2146803C1 |
Authors
Dates
1997-09-10—Published
1995-12-08—Filed