Liu, S., Wang, K. & Abel, D. Robust state and protection-level estimation within tightly coupled GNSS/INS navigation system. GPS Solut 27, 111 (2023). https://doi.org/10.1007/s10291-023-01447-z
In autonomous applications for mobility and transport, a high-rate and highly accurate vehicle-state estimation is achieved by fusing measurements of global navigation satellite systems (GNSS) and inertial sensors. The state estimation and its protection-level generation often suffer from satellite-signal disturbances in urban environments and subsequent poor parametrization of the satellite observables. Thus, we propose an innovative scheme involving an extended H_infinity filter (EHF) for robust state estimation and zonotope for the protection-level generation. This scheme is shown as part of a tightly coupled navigation system based on an inertial navigation system and aided by the GPS/Galileo dual-constellation satellite navigation system. Specifically, GNSS pseudorange and deltarange observables are utilized. The experimental results of post-processing a real-world dataset show significant advantages of EHF against a conventional extended Kalman filter regarding the navigation accuracy and robustness under various GNSS-measurement parametrizations and environmental circumstances. The zonotope-based protection-level calculation is proven valid, computationally affordable, and feasible for real-time implementations.
Real-time tightly coupled GNSS and IMU integration via Factor Graph Optimization
University Politehnica of Bucharest(巴特亚大学);Three Tensors S.R.L.(Three Tensors公司);University of Bucharest(布加勒斯特大学);Navigation Systems Definition Section (TEC-SEN), ESA(欧洲航天局导航系统定义部门);Romanian InSpace Engineering S.R.L. (RISE)(罗马尼亚InSpace工程公司)
Seq-DeepIPC: Sequential Sensing for End-to-End Control in Legged Robot Navigation
Department of Computer Science and Electronics, Universitas Gadjah Mada(计算机科学与电子系,加查马达大学);Department of Computer Science and Engineering, Toyohashi University of Technology(计算机科学与工程系,东福冈技术大学)