This invention relates to a lightweight, miniaturized 3S configuration triaxial integrated
fiber-MEMS
inertial measurement unit, belonging to the field of measurement devices. It includes a base cover, a power supply and detection board
assembly located on the top of the base cover, a
light source assembly located above the power supply and detection board
assembly, a MEMS assembly mounted above the
light source assembly, a base fixed to the base cover,
fiber optic ring assemblies fixed to the base, and a
reference mirror fixed to the top of the base. The power supply and detection board assembly, the
light source assembly, and the MEMS assembly are all arranged inside the base. The three
fiber optic ring assemblies are evenly distributed on a
conical surface with an outer half-cone angle of 54.74° and a bottom projection of 120°. The light source assembly shares a light source with the three fiber optic ring assemblies via a 1*3 coupler. This invention eliminates the unnecessary space occupied by the traditional three independent light source configuration, reduces the overall volume, and improves
optical path consistency and
system stability. It can meet the
engineering requirements of commercial
satellite platforms for the
miniaturization and
mass production of inertial measurement components.