Pugazhenthi Sivasankar , Bennie G. Lewis Jr. , Austin B. Probe , Tarek A. Elgohary
{"title":"一种应用于正交概率逼近的轨道不确定性传播验证框架","authors":"Pugazhenthi Sivasankar , Bennie G. Lewis Jr. , Austin B. Probe , Tarek A. Elgohary","doi":"10.1016/j.actaastro.2025.02.034","DOIUrl":null,"url":null,"abstract":"<div><div>This paper presents a validation framework using data for uncertainty propagation techniques for space situational awareness (SSA) applications. In particular, we validate a novel technique for uncertainty propagation, dubbed here as Orthogonal Probability Approximation (OPA) This technique describes the evolution of state/parameter uncertainties, e.g. initial condition and/or drag coefficient, of nonlinear dynamical systems at a future time. This new uncertainty quantification method employs Liouville’s theorem and Chebyshev polynomial approximation to create a functional representation of the probability density function (PDF) at the future time of interest at a fraction of the computational cost of classical high-fidelity uncertainty propagation methods. OPA is first compared against Polynomial Chaos Expansions and Monte-Carlo simulations to numerically demonstrate the accuracy of the method. For the real data validation, two sources of satellite data are used: GRACE navigation data from the Jet Propulsion Laboratory (JPL) database, and FireOPAL ground-based observer provided by Lockheed Martin. In the presented validation framework, the state/parameter uncertainties of resident space objects (RSOs) are propagated by OPA without using any measurements. The maximum likelihood estimate and the uncertainty bounds of the RSO state from OPA are compared with documented estimates and uncertainty bounds obtained from real satellite/object tracking data as well as other uncertainty propagation methods Results indicate successful validation using GRACE navigation data (precise orbit determination in LEO), and FireOPAL sensor tracking data for Yamal 202 (GEO case) and a rocket body of Block-DM satellite with highly elliptical orbit (HEO). The results show the capability of OPA to accurately estimate the states of RSOs in the absence of continuous measurements, and, in addition, the presented framework can be used to validate any uncertainty propagation technique.</div></div>","PeriodicalId":44971,"journal":{"name":"Acta Astronautica","volume":"232 ","pages":"Pages 453-478"},"PeriodicalIF":3.1000,"publicationDate":"2025-03-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"A validation framework for orbit uncertainty propagation using real satellite data applied to orthogonal probability approximation\",\"authors\":\"Pugazhenthi Sivasankar , Bennie G. Lewis Jr. , Austin B. Probe , Tarek A. Elgohary\",\"doi\":\"10.1016/j.actaastro.2025.02.034\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>This paper presents a validation framework using data for uncertainty propagation techniques for space situational awareness (SSA) applications. In particular, we validate a novel technique for uncertainty propagation, dubbed here as Orthogonal Probability Approximation (OPA) This technique describes the evolution of state/parameter uncertainties, e.g. initial condition and/or drag coefficient, of nonlinear dynamical systems at a future time. This new uncertainty quantification method employs Liouville’s theorem and Chebyshev polynomial approximation to create a functional representation of the probability density function (PDF) at the future time of interest at a fraction of the computational cost of classical high-fidelity uncertainty propagation methods. OPA is first compared against Polynomial Chaos Expansions and Monte-Carlo simulations to numerically demonstrate the accuracy of the method. For the real data validation, two sources of satellite data are used: GRACE navigation data from the Jet Propulsion Laboratory (JPL) database, and FireOPAL ground-based observer provided by Lockheed Martin. In the presented validation framework, the state/parameter uncertainties of resident space objects (RSOs) are propagated by OPA without using any measurements. The maximum likelihood estimate and the uncertainty bounds of the RSO state from OPA are compared with documented estimates and uncertainty bounds obtained from real satellite/object tracking data as well as other uncertainty propagation methods Results indicate successful validation using GRACE navigation data (precise orbit determination in LEO), and FireOPAL sensor tracking data for Yamal 202 (GEO case) and a rocket body of Block-DM satellite with highly elliptical orbit (HEO). The results show the capability of OPA to accurately estimate the states of RSOs in the absence of continuous measurements, and, in addition, the presented framework can be used to validate any uncertainty propagation technique.</div></div>\",\"PeriodicalId\":44971,\"journal\":{\"name\":\"Acta Astronautica\",\"volume\":\"232 \",\"pages\":\"Pages 453-478\"},\"PeriodicalIF\":3.1000,\"publicationDate\":\"2025-03-11\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Acta Astronautica\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0094576525001158\",\"RegionNum\":2,\"RegionCategory\":\"物理与天体物理\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Acta Astronautica","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0094576525001158","RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
A validation framework for orbit uncertainty propagation using real satellite data applied to orthogonal probability approximation
This paper presents a validation framework using data for uncertainty propagation techniques for space situational awareness (SSA) applications. In particular, we validate a novel technique for uncertainty propagation, dubbed here as Orthogonal Probability Approximation (OPA) This technique describes the evolution of state/parameter uncertainties, e.g. initial condition and/or drag coefficient, of nonlinear dynamical systems at a future time. This new uncertainty quantification method employs Liouville’s theorem and Chebyshev polynomial approximation to create a functional representation of the probability density function (PDF) at the future time of interest at a fraction of the computational cost of classical high-fidelity uncertainty propagation methods. OPA is first compared against Polynomial Chaos Expansions and Monte-Carlo simulations to numerically demonstrate the accuracy of the method. For the real data validation, two sources of satellite data are used: GRACE navigation data from the Jet Propulsion Laboratory (JPL) database, and FireOPAL ground-based observer provided by Lockheed Martin. In the presented validation framework, the state/parameter uncertainties of resident space objects (RSOs) are propagated by OPA without using any measurements. The maximum likelihood estimate and the uncertainty bounds of the RSO state from OPA are compared with documented estimates and uncertainty bounds obtained from real satellite/object tracking data as well as other uncertainty propagation methods Results indicate successful validation using GRACE navigation data (precise orbit determination in LEO), and FireOPAL sensor tracking data for Yamal 202 (GEO case) and a rocket body of Block-DM satellite with highly elliptical orbit (HEO). The results show the capability of OPA to accurately estimate the states of RSOs in the absence of continuous measurements, and, in addition, the presented framework can be used to validate any uncertainty propagation technique.
期刊介绍:
Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to:
The peaceful scientific exploration of space,
Its exploitation for human welfare and progress,
Conception, design, development and operation of space-borne and Earth-based systems,
In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.