FIELD: aviation.
SUBSTANCE: group of inventions relates to method and system of coarse control of spatial movement of aircraft. To control spatial movement of aircraft, signals of setting angle of roll and yaw are generated, angles of roll, yaw and pitch are measured, generating control signals on angle of roll and yaw, signals of difference between reference signals of roll and yaw and measured signals on angle of roll and yaw respectively, obtained difference signals are separately integrated, differentiated, scaled and first difference signal is summed with roll angle control signal, second difference signal with pitch angle control signal. Coarse control system comprises devices for setting angles of roll and yaw, two controllers, two actuators, sensors of roll, yaw and pitch angles, two reference models, six amplifiers, four adders, two differentiators, two integrators, connected in a certain manner.
EFFECT: providing stability of movement under non-stationary flight parameters and effect of adaptive noise.
2 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF SPACECRAFT SPATIAL ORIENTATION CONTROL AND CONTROL SYSTEM FOR ITS IMPLEMENTATION | 2016 |
|
RU2618856C1 |
SYSTEM FOR ADAPTIVE CONTROL OF AEROPLANE ON PITCH ANGLE | 2010 |
|
RU2445671C2 |
METHOD AND APPARATUS FOR CONTROLLING PILOT-NAVIGATION SYSTEM | 2010 |
|
RU2440595C1 |
SYSTEM OF CONTROL OF ANGULAR MOTION OF AIRCRAFT WITH STATIC DRIVE | 2007 |
|
RU2335009C1 |
APPARATUS FOR MONITORING INERTIAL NAVIGATION SYSTEM | 2013 |
|
RU2536365C1 |
SYSTEM OF CONTROL OF ANGULAR MOTION OF AIRCRAFT WITH STATIC DRIVE | 2007 |
|
RU2335006C1 |
AUTOMATIC CONTROL SYSTEM FOR UNMANNED AIRCRAFT ON ANGLE OF SEARCH | 2016 |
|
RU2675976C2 |
METHOD FOR CONTROLLING INFRARED VERTICAL EARTH SENSOR WITH AUTOMATIC CIRCULAR SCAN ANGLE ADJUSTMENT | 2023 |
|
RU2814305C1 |
METHOD OF CONTROL OF ANGULAR MOTION OF AIRCRAFT WITH INTEGRATING DRIVE | 2007 |
|
RU2335005C1 |
METHOD AND DEVICE FOR CONTROLLING HORIZONTAL ORIENTATION OF AIRCRAFT | 2007 |
|
RU2373562C2 |
Authors
Dates
2016-06-20—Published
2014-10-03—Filed