A novel constrained skew-Gaussian filter and its application to maneuverable reentry vehicle tracking

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Wang Ruipeng, Wang Xiaogang
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Abstract

The state of the system generally satisfies specific constraints imposed by material properties or physical laws, so the application of these constraints can improve the accuracy of state estimation. In this paper, a novel recursive filter referred as constrained high-degree cubature skew-Gaussian filter (CHCSGF) is proposed, which achieves soft-constrained state estimation by compressing the probability density of unconstrained states with constraint information. First, the probability density of the state under inequality soft constraints is modeled as a skew-Gaussian (SG) distribution, rather than truncated or single Gaussian distributions. Then, a recursive constrained SG filter is developed to handle inequality soft constraints in linear systems. Addressing nonlinear challenges, a 5th-degree spherical-radial cubature approximation method is presented to numerically calculate SG-weighted integrals for the nonlinear transformation of SG distribution. Finally, the CHCSGF algorithm is proposed using this method to tackle nonlinear filtering problems. The CHCSGF is applied to reentry trajectory tracking to improve estimation accuracy by dealing with heat flow, dynamic pressure and overload constraints during reentry flight. Simulation results demonstrate that the CHCSGF achieves higher estimation accuracy than unconstrained methods under nonlinear inequality soft constraints, and is robust to the constraints with a prior error. Compared to particle filter and moving horizon estimation, the computational complexity of CHCSGF is significantly reduced.

Abstract Image

新型约束偏高斯滤波器及其在机动再入飞行器跟踪中的应用
系统的状态通常满足材料特性或物理规律施加的特定约束,因此应用这些约束可以提高状态估计的精度。本文提出了一种新型递归滤波器,即约束高阶立方体偏高斯滤波器(CHCSGF),它通过利用约束信息压缩无约束状态的概率密度来实现软约束状态估计。首先,不等式软约束下的状态概率密度被建模为偏高斯(SG)分布,而不是截断分布或单一高斯分布。然后,开发了一种递归约束 SG 滤波器,用于处理线性系统中的不平等软约束。针对非线性挑战,提出了一种 5 度球面-径向立方近似方法,用于数值计算 SG 分布非线性变换的 SG 加权积分。最后,利用该方法提出了 CHCSGF 算法,以解决非线性滤波问题。CHCSGF 被应用于再入轨道跟踪,通过处理再入飞行过程中的热流、动态压力和过载约束来提高估计精度。仿真结果表明,在非线性不等式软约束条件下,CHCSGF 比无约束方法获得了更高的估计精度,并且对具有先验误差的约束条件具有鲁棒性。与粒子滤波和移动地平线估计相比,CHCSGF 的计算复杂度大大降低。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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