2025-12-15
MEMS (Micro-Electro-Mechanical Systems) Inertial Navigation System is a high-precision navigation device manufactured based on micro-electro-mechanical technology. It is mainly composed of MEMS gyroscopes (for measuring angular velocity), MEMS accelerometers (for measuring acceleration) and data processing units. Without relying on external references such as satellite signals or ground base stations, it can independently calculate position, velocity and attitude information by sensing its own motion state. This "autonomous navigation" feature makes it an ideal choice for the extreme environment of space.
Compared with traditional aerospace-grade inertial navigation systems, MEMS inertial navigation boasts three core advantages: miniaturization, lightweight design and low cost. Its core components can be reduced to millimeter scale, with a weight ranging from several grams to tens of grams and power consumption as low as milliwatt level. Moreover, it can be mass-produced, perfectly meeting the core demand of spacecraft for "weight reduction and efficiency improvement". Meanwhile, after special reinforcement treatments such as radiation resistance and high-low temperature resistance, MEMS inertial navigation can withstand extreme space conditions including vacuum, strong radiation and drastic temperature variations (-200℃~+120℃), with its stability and reliability reaching aerospace-grade standards.
Satellites need to accurately maintain their attitude during orbital operation (e.g., aligning solar panels with the sun and communication antennas with the Earth), a task primarily accomplished by MEMS inertial navigation systems. By real-time measuring the angular velocity and attitude changes of satellites, it provides data support for the attitude control system, driving actuators such as thrusters and reaction wheels to adjust the attitude in a timely manner and ensure the stable operation of satellites.
For instance, in low-Earth orbit communication satellite constellations (such as Starlink), each satellite needs to quickly complete orbital switching and attitude calibration. MEMS inertial navigation has become the core navigation component for the batch deployment of constellations due to its advantages of "fast response and small size". For deep-space probes (such as Mars rovers and asteroid detectors), real-time navigation relying on ground telemetry signals is impossible in the deep space far away from the Earth. MEMS inertial navigation, combined with star trackers and atomic clocks, forms an autonomous navigation system to ensure the probe accurately flies to the target celestial body.
In manned spacecraft such as manned spaceships and space stations, MEMS inertial navigation undertakes a "life-support level" critical mission. It not only can real-time monitor the attitude, velocity and position of the spacecraft, providing accurate data for orbital adjustment and rendezvous and docking, but also can quickly trigger the emergency attitude control program in case of emergencies (such as docking failure between the spaceship and the space station, or abnormal attitude of the return capsule during re-entry into the atmosphere), thus ensuring the safety of astronauts.
Taking the Shenzhou spaceship as an example, when the return capsule re-enters the atmosphere, it will experience intense aerodynamic heating and attitude disturbance. MEMS inertial navigation, working in coordination with infrared navigation and parachute control systems, accurately calculates the position and attitude of the return capsule to ensure it lands safely at the predetermined landing site. In addition, a miniature MEMS inertial navigation module is integrated into the astronauts' extravehicular spacesuits, which real-time monitors the astronauts' motion attitude and provides navigation reference for extravehicular activities.
With the development of space on-orbit service technologies (such as satellite maintenance, space debris removal and on-orbit assembly), space robots (robotic arms and autonomous mobile robots) have become core equipment, and MEMS inertial navigation is the key to their "precision operation". It can real-time sense the joint motion and position deviation of robots, ensuring the robotic arm accurately grabs satellites, completes equipment replacement, or enables the mobile robot to move along the predetermined path outside the space station cabin.
For example, when the robotic arm of the International Space Station (ISS) transfers astronauts and transports cargo, the high-precision attitude data provided by MEMS inertial navigation can control the operation error within centimeter level. In the future, when "space tugs" clean up space debris, they need to accurately dock with the debris, and the autonomous navigation capability of MEMS inertial navigation can ensure a stable and reliable docking process.
In deep-space exploration missions such as lunar and Mars exploration, ground telemetry signals have a delay of several minutes or even tens of minutes, making real-time control of the probe impossible. The "autonomous navigation" feature of MEMS inertial navigation is thus particularly important. Integrated with optical navigation, radar navigation and other technologies, it forms a multi-source fusion navigation system, enabling the probe to independently plan paths, avoid obstacles and achieve precise landing.
For instance, when the Chang'e-5 lunar probe conducted lunar surface sampling, MEMS inertial navigation real-time monitored the attitude and position of the probe, ensuring the sampling robotic arm accurately positioned the target area. When the Mars rover travels on the Martian surface, MEMS inertial navigation, combined with terrain camera data, independently adjusts the traveling direction and speed to avoid getting stuck in sand dunes or colliding with rocks.
The application of MEMS inertial navigation in the space field is inseparable from two core technological breakthroughs. First is precision improvement. By adopting new materials (such as silicon-based microstructures and quartz crystals) and signal processing algorithms (such as Kalman filtering and neural network compensation), the bias stability of MEMS gyroscopes has reached the level of 0.01°/h, which is close to that of traditional fiber optic inertial navigation systems. Second is reinforcement for extreme environments. Through optimized packaging technology and radiation shielding design, MEMS inertial navigation can operate stably for a long time in the harsh space radiation environment, with a service life of more than 10 years.
In the future, the application of MEMS inertial navigation in the space field will develop in three directions. First is miniaturization and integration, integrating functions such as navigation, communication and energy supply onto a single chip to create "on-chip spacecraft". Second is multi-source fusion navigation, achieving in-depth integration with star trackers, atomic clocks, quantum navigation and other technologies to further improve navigation accuracy and reliability. Third is deep-space expansion, being applied to farther space missions such as asteroid exploration and interstellar navigation, and becoming the "portable navigation brain" for human beings to explore the universe.
From satellite attitude control to manned spaceflight safety guarantee, from deep-space exploration autonomous navigation to space robot precision operation, MEMS inertial navigation is reshaping the navigation mode of space exploration with its characteristics of "miniaturization, autonomy and high reliability". With the continuous advancement of technology, this "miniature navigation brain" will provide solid navigation support for human beings to explore the unknown in more distant cosmic journeys, helping space exploration enter a new era of higher efficiency, lower cost and greater safety.
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