A SINS/BDS Integrated Navigation Method Based on Classified Weighted Adaptive Filtering
Author:
Affiliation:
1. Graduate College, Air Force Engineering University, Xi’an, China
2. Air and Missile Defense College, Air Force Engineering University, Xi’an, China
Abstract
Funder
National Natural Science Foundation of China
Publisher
Hindawi Limited
Subject
General Engineering,General Mathematics
Link
http://downloads.hindawi.com/journals/mpe/2019/2158351.pdf
Reference11 articles.
1. A landmark-based navigation method for autonomous aircraft
2. Adaptive GPS/INS integration for relative navigation
3. An innovative transfer alignment method based on federated filter for airborne distributed POS
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1. In-Flight Alignment Method of SINS/GPS Integrated Navigation System Based on IUKF;Lecture Notes in Electrical Engineering;2021-10-06
2. SINS/BDS Integrated Navigation for Hypersonic Boost-Glide Vehicles in the Launch-Centered Inertial Frame;Mathematical Problems in Engineering;2020-11-12
3. The robust residual-based adaptive estimation Kalman filter method for strap-down inertial and geomagnetic tightly integrated navigation system;Review of Scientific Instruments;2020-10-01
4. Application of Improved Simplex Quadrature Cubature Kalman Filter in Nonlinear Dynamic System;Mathematical Problems in Engineering;2020-05-14
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