This invention discloses a lightweight, compact, three-axis integrated
fiber optic inertial navigation device, belonging to the field of inertial navigation technology. Specifically, it relates to a lightweight, compact, three-axis integrated
fiber optic inertial navigation device, comprising a housing, an
inertial measurement unit (IMU), a magnetic shielding plate, and navigation
control circuit components. The IMU includes three orthogonally arranged accelerometers, three orthogonally arranged
fiber optic loop components, and an SLD (Single-Loop
Light Source). The three fiber optic loop components share a single SLD
light source, forming a three-axis integrated fiber optic
gyroscope. The fiber optic loop components include a loop support, a 260m polarization-maintaining fiber optic loop, and a
magnetic shield. The
magnetic shield is fixed to the lower end face of the loop support, forming a closed magnetic shielding environment. The 260m polarization-maintaining fiber optic loop is located within this closed magnetic shielding environment. This invention optimizes the design of the IMU and navigation
control circuit components of the fiber optic
inertial navigation system, achieving magnetic shielding isolation of the fiber optic loop and physical isolation of heat-generating devices while reducing
system weight and volume, thereby improving the stability of the
navigation system.