FIELD: space engineering. SUBSTANCE: proposed device has three mutually perpendicular circuits, three-component accelerometer, three-component magnetic field ferroprobe sensor, microprocessor and controllable source. Accelerometer and ferroprobe sensor are connected with inputs of microprocessor whose outputs are connected with in puts of controllable source of current whose outputs are connected in series with current-carrying circuits located on outer surface of spacecraft. Circuits are provided with magnetic screens. EFFECT: reduction of range of microaccelerations arising on board; enhanced accuracy of compensation slowly changing accelerations and about change in accelerations caused by operation of on-board equipment. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR LOCATING AIR LEAKAGE IN SPACE VEHICLE MODULES | 2000 |
|
RU2189074C2 |
ELECTRIC CAPACITY LEVER INDICATOR | 2000 |
|
RU2178549C2 |
GAS TURBINE BLADE | 2000 |
|
RU2178086C2 |
PROCEDURE ESTABLISHING ANGULAR POSITIONS OF BLADES OF TURBOMACHINES ( VARIANTS ) | 2002 |
|
RU2215986C1 |
SMOKINESS CONTROLLER OF WASTE GASES OF HEAT POWER INSTALLATIONS | 2001 |
|
RU2210759C1 |
TECHNIQUE DETERMINING DIRECTION OF VECTOR OF INDUCTION OF MAGNETIC FIELD IN IONOSPHERE OF THE EARTH AND GEAR FOR ITS REALIZATION | 1999 |
|
RU2169933C2 |
DEVICE WARNING OF PREEMERGENCY DEFORMATION OF BLADES OF TURBO-MACHINE | 2000 |
|
RU2177145C1 |
GEAR FOR ELECTRIC DISCHARGE TREATMENT OF AIR IN SMALL-SIZED CLOSED VOLUMES | 1999 |
|
RU2173666C2 |
METHOD DETERMINING DEFORMATION OF BLADES OF ROTATING WHEEL OF TURBO-MACHINE AND GEAR FOR ITS IMPLEMENTATION | 1998 |
|
RU2152590C1 |
METHOD FOR CALIBRATION OF ACCELERATION SENSOR IN SPACE FLIGHT | 2014 |
|
RU2583882C1 |
Authors
Dates
2002-07-20—Published
2000-06-02—Filed