Guidance Law Design for a Class of Dual-Spin Mortars

Author:

Guo Qing-wei1,Song Wei-dong1,Wang Yi1,Lu Zhi-cai1

Affiliation:

1. The Electrical Engineering Department, Shijiazhuang Mechanical Engineering College, Shijiazhuang 050003, China

Abstract

To minimize the cost and maximize the ease of use, a class of dual-spin mortars is designed which only rely on GPS receiver and geomagnetic measurements. However, there are some problems to be solved when the range is small, such as low correction authority and trajectory bending. Guidance law design for this mortar is detailed. Different guidance laws were designed for the ascending and descending segments, respectively. By taking variable parameter guidance law in the vertical plane and using compensation in the lateral plane, the problems mentioned above were resolved. Roll angle resolving algorithms with geomagnetic measurements were demonstrated and the experiment results proved to be effective. In order to verify the effectiveness, Seven-Degrees-of-Freedom (7-DOF) rigid ballistic model were established and hardware in the loop simulation was introduced. After the transform function of the actuator was obtained, the control model of the shell was improved. The results of the Monte Carlo simulation demonstrate that the guidance law is suitable and the mortar can be effectively controlled.

Publisher

Hindawi Limited

Subject

Aerospace Engineering

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Three-Dimensional Guidance Law Mimicking Realistic Ballistic Trajectories;Journal of Guidance, Control, and Dynamics;2022-09

2. A novel quasi-dynamic guidance law for a dynamic dual-spin projectile with non-conventional, asymmetric roll constraints;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-03-01

3. Optimization of the PNG Law for a Dual-Spin Mortar with Fixed Canards;Mathematical Problems in Engineering;2021-11-02

4. Piecewise Prediction Control Design for a Class of Spin-Stabilized Projectiles in Descending Segment;2021 China Automation Congress (CAC);2021-10-22

5. Research on Control Force Aerodynamic Model of a Guided Rocket With an Isolated-rotating Tail Rudder;International Journal of Aeronautical and Space Sciences;2021-09-24

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