Precision Constellation Position Determination, Phase I

For a distributed aperture sensor, especially at infrared and optical wavelengths, the relative position of the aperture components must be known and controlled precisely. When the aperture components are on separate independent spacecraft, determining the relative range and bearing is the challenge our proposed innovation addresses. The estimation of the relative range and bearing will be used in the positioning and control of remote sensors. Using a laser cross-link between the spacecraft, the fine positioning (25 cm) stage can be accomplished using the network protocols, message structure and by leveraging a balanced system of range and synchronization we have developed and employed on experimental and operational systems. For hyperfine position (1 micron) we propose to use the same cross-link since the laser wavelength is the same size as the requirement. Tuning is accomplished by setting up an interference pattern between the two satellite laser beams and adjusting the focal plane for the maximum intensity. To solve the phase ambiguity that will arise, we propose to further modulate the lasers with a pseudo-random noise code and integrate over several code chip intervals to resolve the ambiguity and reach the 1 micron requirement.

This is a mature technology (TRL 7+) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.

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