FIELD: aviation instrument engineering, in particular, control systems providing for by-pass of obstacles, terrain features by flight vehicles in a low-altitude flight. SUBSTANCE: the control system uses a coordinate and speed transducer, first difference unit, lateral deviation parameters setter. In addition, use is made of a closed loop parameters setter, prediction signal generating unit and a control signal and parametric derivatives generating unit. EFFECT: enhanced accuracy. 3 cl, 4 dwg
Title | Year | Author | Number |
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FLIGHT ALTITUDE CONTROL SYSTEM | 1994 |
|
RU2081396C1 |
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RU2098322C1 |
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INFORMATION SYSTEM FOR FORMATION OF ABSOLUTE ALTITUDE | 1994 |
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INFORMATION SYSTEM OF INTER-AIRCRAFT NAVIGATION | 1995 |
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FLYING VEHICLE LATERAL MOVEMENT CONTROL SYSTEM | 1996 |
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COMPLEX INERTIAL SYSTEM | 1996 |
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FLIGHT ALTITUDE CONTROL SYSTEM | 1996 |
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SYSTEM FOR CONTROL OF FLIGHT ALTITUDE AT LANDING | 1996 |
|
RU2102281C1 |
Authors
Dates
1997-05-10—Published
1994-05-31—Filed