Discrete Event Command and Control for Formation Flying of Distributed Small Spacecraft Systems

A distributed, multi-vehicle concept for future space missions has been conceived as a solution to the problem of advancing space-based operations within budgetary constraints. Broadly named formation flying, this approach to designing distributed systems across multiple, spatially disbursed platforms is enabled by collectively coordinating a fleet of autonomous spacecraft to function as a unified system. Formation flying offers potential advantages of improved robustness, capability, and cost relative to complicated, single platform systems by using multiple, often small, spacecraft to perform complex multi-sensor tasks. A necessary element in the realization of formation flying systems is the development of methods and technologies that facilitate the transition from treating a distributed spacecraft system as individual elements, to viewing a formation as a coordinated system unified by common objectives. This paper describes the results of research performed to identify fundamental issues that affect the development of command and control (C) methods applicable to coordinating distributed small spacecraft systems. A discrete event method of distributed command and control is described that is particularly well suited to small spacecraft formation flying. Utilized in many complex terrestrial systems, discrete event systems (DES) concepts facilitate coordination of distributed systems at multiple levels of resolution in an efficient manner. DES also provide a means to integrate intelligent planning and processing operations while interfacing with more traditional subsystem controllers. The basic principals and applicability of DES are described within the context of formation flying and example distributed spacecraft C operations are defined.