METHOD AND DEVICE FOR PROTECTION OF SPACE COMPLEXES WHEN CONDUCTING ACTIVE EXPERIMENTS

摘要

The method and the device can be applied in space research, in particular for the intensity of the electric fields, the potential of the body of the space flying machine and the parameters of space plasma by continuous monitoring and analysis of the parameters of the space medium. The device for the protection of space complexes during conducting active experiments comprises sensor units (1Æ, 1öà1n), the outputs of which are included in the respective inputs of adaptive units (2Æ, 2öà2n). The other inputs of units (2Æ, 2öà2n) are coupled to the respective outputs of control unit (3). The outputs of adaptive units (2Æ, 2öà2n) are connected to the respective inputs of the unit for input signals processing (4), the output on its part being coupled to a unit for analysis of the characteristics of the amplitudes of these signals (5). The output of the signal analysis unit (5) is connected to the input of the unit for synthesizing of control signals (6), the output of unit (6) being coupled to the first input of the unit for adaptive units control (3). The other output of unit (6) is connected to a unit for the protection and control of device (7), one of the outputs of which is connected to the input of the common protection unit (8) of the entire apparatus complex on board of the space flying machine, and the other one û to the second input of the control unit (3).