Gain-scheduled extended Kalman filter for nanosatellite attitude determination system

Extended Kalman filter (EKF) has been widely used for attitude determination in various satellite missions. However, it requires an extensive computational power which is not suitable for nano-satellite application. This paper proposes a gain-scheduled EKF (GSEKF) to reduce the computational require...

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Bibliographic Details
Main Authors: Pham, Minh Duc, Low, Kay Soon, Goh, Shu Ting, Chen, Shoushun
Other Authors: School of Electrical and Electronic Engineering
Format: Article
Language:English
Published: 2015
Subjects:
Online Access:https://hdl.handle.net/10356/79372
http://hdl.handle.net/10220/38331
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Institution: Nanyang Technological University
Language: English