Abstract

The projectile-borne data recorder is used to measure and record the position and attitude data of exterior ballistic flights, which experience high overload during the launching process. The navigation algorithm can be optimized by analyzing the data stored in the recorder. As the primary means of acquiring the navigation data, the micro inertial measurement unit (MIMU) is an inevitable part of the projectile equipment. However, its mechanical structure could hardly bear the high overload during operation. In view of the above problems, a novel projectile-borne data recorder triggered by overload is designed in this paper. The recorder could have the navigation system powered when the projectile leaves the barrel so as to activate the data recording of the high overload. Furthermore, the viability of the MIMU of the high overload is guaranteed through a specific way of system encapsulation. In the proposed design, the overload switch redundancy and the power supply redundancy were adopted to improve reliability. The proposed design is tested with practical experiments, and the results show that the proposed recorder could be effectively triggered by overloading, and the supply voltage is stable, which helps record reliable data for the projectile.

Highlights

  • The intelligent projectile is amongst the guided weapons that are fired by an artillery and strike the target accurately through searching, guidance and control during flight [1]

  • This paper aims to design a flight recorder for the projectile, to record the miniature inertial measurement unit (MEMS-IMU) data in real time, and protect the mechanical systems (MEMS)-IMU from being damaged under the great impact

  • The Machete hammer is used in the laboratory to generate the impact acceleration so as to simulate the projectile launching circumstance, in which, the supply stability of the power supply module, the reliability of the impact detection and the effectiveness of the recording function are validated

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Summary

Introduction

The intelligent projectile is amongst the guided weapons that are fired by an artillery and strike the target accurately through searching, guidance and control during flight [1]. Use in the EX-171 extended range guided munition [2], the combination of the micro inertial measurement unit (MIMU). GPS, is a popular scheme for attitude measurement and control [2,3], where the MIMU constituting of the tri-axial accelerometers and gyroscopes, is a sensor unit for measuring acceleration, tilt, impact, vibration, rotation. The spacing of the comb tooth structure is very small (about 10 μm) in the high-precision micro electro-mechanical systems (MEMS) gyroscope, and there would be resonant vibration with high frequency and large amplitude (1–3 μm) in the comb tooth structure when the power is on, so the device is more likely to fail under great impact [5]. The impact acceleration is large, with an intensity of more than

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