A gravity
gradiometer is combined with a two-stage actively controlled
isolation system. The gravity
gradiometer and two stage
isolation system may then be mounted within (or on) a
mobile vehicle such as, for example, an aircraft. It has been recognized by the inventors herein that the accelerations imparted to an aircraft during normal operations can be separated through
system design into two relatively distinct regimes within the
frequency domain. The invention provides a first isolation
mount, which forms part of the
isolation system, to isolate accelerations (and resulting translations) falling within a first of the two frequency regimes. The second isolation
mount, which is mounted to the first isolation
mount, isolates accelerations falling within the second of the two frequency regimes. A gravity
gradiometer can then be mounted to the second isolation mount. As a result of housing the gravity gradiometer within the nested isolation
system (a combination of the first and second isolation mounts), the gravity gradiometer is substantially isolated from the accelerations experienced by the
mobile vehicle. Consequently, gravity gradients measured by the gravity gradiometer are relatively
noise free and provide heretofore-unobtainable accuracy.