Model Predictive Tracking Control With Parameter Estimation for Spin-Stabilized Indirect Fire Symmetric Projectiles

Author:

Nash Austin L.1

Affiliation:

1. Rose-Hulman Institute of Technology Mechanical Engineering Department, , Terre Haute, IN 47803

Abstract

Abstract Impact point prediction, estimation, and control is a critical component of many smart weapons applications. In this work, I propose a method for estimating and controlling impact points of indirect fire launches for a spin-stabilized symmetric projectile with forward-mounted canard actuators. My method uses an algebraic point mass model to enable parameter estimation for time-varying parameters within a separate linear prediction model that can be leveraged for real-time impact point control. The point mass model also serves as the basis for a reference trajectory for any launch condition and thus eliminates the need for obtaining preloaded reference trajectories. I then use a linear prediction model in conjunction with the parameter estimates to synthesize a linear MPC tracking control algorithm for projectile impact point control. The MPC tracking controller allows incorporation of actuator saturation constraints and is shown to successfully guide a set of indirect fire launches toward a desired downrange target. A comparative case study to existing work in the literature shows that the proposed method results in a 56% reduction in the CEP radius, which is a prescribed radius such that half of the points of a given set lie within the circle, for a set of 50 yaw and pitch launch angle pairs.

Publisher

ASME International

Subject

General Medicine,General Chemistry

Reference9 articles.

1. Theory, Guidance, and Flight Control for High Maneuverability Projectiles;Fresconi,2014

2. Linear Theory of a Dual-Spin Projectile in Atmospheric Flight;Costello;J. Guidance Control Dyn.,2000

3. Impact Point Model Predictive Control of a Spin-Stabilized Projectile With Instability Protection;Gross;Proc. Inst. Mech. Eng. Part G: J. Aerosp. Eng.,2014

4. Model Predictive Lateral Pulse Jet Control of an Atmospheric Rocket;Burchett;J. Guidance Control Dyn.,2002

5. A Comparison of Different Guidance Schemes for a Direct Fire Rocket With a Pulse Jet Control Mechanism;Burchett,2002

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3