Development contract for the DSP-based Vibration Control Electronics (VCE) circuit card assembly. The purpose of the VCE is to demonstrate vibration isolation, suppression, steering capabilities, and their benefits to optical payloads during space flight.

A combination of passive and active vibration isolation is achieved via a three axis magnetic voice coil hexpod configuration. This radiation-hardened design is based on the TI TMS320C31 Digital Signal Processor and includes RS485 and 1553 interfaces, FLASH and SRAM memory, and various A/D sensor interfaces. The contract included delivery of two engineering prototypes and one flight ready CCA.