Abstract

Inertial navigation systems based on microelectromechanical systems (MEMS) sensors offer advantages that include small size, light weight, low power consumption, strong environmental adaptability, ...

Highlights

  • Modern warfare requires weapons and military equipment to have characteristics that include a high degree of informatization, high guidance precision, and a high combat efficiency-to-cost ratio

  • Microinertial sensors offer the advantages of small size, light weight, highimpact resistance, low power consumption, and low cost

  • When combined with satellite positioning systems, microinertial sensors have the advantages of the full autonomy of the inertial navigation system, and have the high-precision positioning characteristics

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Summary

Introduction

Modern warfare requires weapons and military equipment to have characteristics that include a high degree of informatization, high guidance precision, and a high combat efficiency-to-cost ratio. Given the characteristics described above, the design of the inertial system for guided ammunition should be focused on the design of an anti-high-overload structure, in-flight initial self-alignment of attitude, integrated MEMS/global navigation satellite system (GNSS) navigation, and error calibration and compensation technology for the micro-inertial devices when operating under highly dynamic conditions. In Wei and Zhang’s literature,[10] the quaternion error equation and extended Kalman filter (EKF) technology have been used to provide effective improvements in the alignment accuracy of a strapdown inertial navigation system with a high-precision inertial device at a large misalignment angle. -coordinate system on the n -coordinate system, v^ nin is the angular velocity of the n -system relative to the i -system obtained using the position and velocity calculations; Quaternion matrix q0 Àq1 Àq2 Àq3

Velocity error equation
Position error equation
Inertial device error equation
Concluding remarks

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