High-quality in situ magnetic field measurements are essential to understanding the geophysical processes that couple mass, energy, and momentum throughout near-Earth space and the solar system. This often involves identifying comparably small perturbations due to field-aligned currents or plasma processes from a much larger background field that, unfortunately, is often contaminated by magnetic noise from the host satellite platform. Stray magnetic fields can emanate from the materials used in the construction of the host spacecraft, from attitude control systems such as reaction wheels and magnetorquers, or from the solar panels, batteries, and electrical systems that manage power for the spacecraft subsystems.To mitigate the impact of the interfering fields, magnetometers can be deployed on a boom, increasing the physical separation from the host spacecraft. Historically, very long booms (e.g., >5-m) have been implemented to achieve optimal interference mitigation (Miller, 1979;Smola et al., 1980). For additional interference mitigation potential, a pair of magnetometers has often been used, mounted at different distances along the boom. At a large distance from the source a simple dipole approximation can be fit to the field gradient and subtracted (Ness et al., 1971). However, many recent missions such as Van Allen Probes (Kletzing et al., 2013) and Dellingr (Clagett et al., 2017) have opted for shorter booms (3 and 0.52-m, respectively) to reduce complexity and implementation costs. This reduced boom length tends to place the sensors in the near-field of the magnetic noise