首页 | 本学科首页   官方微博 | 高级检索  
     检索      


Modeling irregular small bodies gravity field via extreme learning machines and Bayesian optimization
Authors:Roberto Furfaro  Riccardo Barocco  Richard Linares  Francesco Topputo  Vishnu Reddy  Jules Simo  Lucille Le Corre
Institution:1. Department of Systems and Industrial Engineering, Department of Aerospace and Mechanical Engineering, University of Arizona, 1127 E. James E. Roger Way, Tucson, AZ 85721, USA;2. Department of Systems and Industrial Engineering, University of Arizona, Tucson, AZ 86721, USA;3. Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139, USA;4. Dipartimento di Scienze e Tecnologie Aerospaziali, Politecnico di Milano, viaLa Masa 34, 20156 Milano, Italy;5. Department of Planetary Science, Lunar and Planetary Laboratory, University of Arizona, 1127 E. James E. Roger Way, Tucson, AZ 85721, USA;6. School of Engineering, University of Central Lancashire, Preston, Lancashire PR1 2HE, UK;7. Planetary Science Institute, 1700 East Fort Lowell, Suite 106, Tucson, AZ 85719, USA
Abstract:Close proximity operations around small bodies are extremely challenging due to their uncertain dynamical environment. Autonomous guidance and navigation around small bodies require fast and accurate modeling of the gravitational field for potential on-board computation. In this paper, we investigate a model-based, data-driven approach to compute and predict the gravitational acceleration around irregular small bodies. More specifically, we employ Extreme Learning Machine (ELM) theories to design, train and validate Single-Layer Feedforward Networks (SLFN) capable of learning the relationship between the spacecraft position and the gravitational acceleration. ELM-base neural networks are trained without iterative tuning therefore dramatically reducing the training time. Analysis of performance in constant density models for asteroid 25143 Itokawa and comet 67/P Churyumov-Gerasimenko show that ELM-based SLFN are able learn the desired functional relationship both globally and in selected localized areas near the surface. The latter results in a robust neural algorithm for on-board, real-time calculation of the gravity field needed for guidance and control in close-proximity operations near the asteroid surface.
Keywords:Extreme learning machine  Gravity modeling  Asteroid
本文献已被 ScienceDirect 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号