论文信息 - THE DESIGN OF A SOFTWARE SYSTEM FOR A SMALL SPACE SATELLITE

THE DESIGN OF A SOFTWARE SYSTEM FOR A SMALL SPACE SATELLITE

An electrical-to-fluidic interface device is disclosed for converting an electrical error signal into a fluidic control force for missile guidance. A poppet valve is electrically activated and pressure aided during operation to rapidly switch the control force in response to the electrical error signal input.

M. Dabrowski

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