FIELD: instrumentation engineering; systems for control of flight at landing on swinging base (air-craft carrier). SUBSTANCE: system includes altitude selector, difference unit, information sensor unit, stabilization circuit, as well as additionally introduced relative altitude forming unit and correction signal forming unit for altitude control relative to movable swinging plane of landing and compensation for disturbing actions. EFFECT: enhanced efficiency. 3 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
FLIGHT ALTITUDE CONTROL SYSTEM | 1994 |
|
RU2081396C1 |
COMPLEX COMPASS SYSTEM | 1996 |
|
RU2098322C1 |
INFORMATION SYSTEM FOR FORMATION OF ABSOLUTE ALTITUDE | 1994 |
|
RU2085851C1 |
INFORMATION LANDING SYSTEM | 1992 |
|
RU2023984C1 |
INFORMATION SYSTEM OF INTER-AIRCRAFT NAVIGATION | 1995 |
|
RU2089449C1 |
FLIGHT VEHICLE LATERAL MOTION CONTROL SYSTEM | 1994 |
|
RU2079108C1 |
COMPLEX NAVIGATION SYSTEM | 1992 |
|
RU2023983C1 |
COMPLEX SIGHTING SYSTEM | 1999 |
|
RU2161777C1 |
COMPLEX INERTIAL SYSTEM | 1996 |
|
RU2089450C1 |
DEVICE FOR MEASUREMENT OF MAGNETIC FIELDS | 1997 |
|
RU2124737C1 |
Authors
Dates
1998-01-20—Published
1996-09-24—Filed