Title :
Low-cost sensors based Multi-Sensor Data Fusion techniques for RPAS Navigation and Guidance
Author :
Cappello, Francesco ; Ramasamy, Subramanian ; Sabatini, Roberto ; Jing Liu
Author_Institution :
Sch. of Aerosp., Mech. & Manuf. Eng., RMIT Univ., Melbourne, VIC, Australia
Abstract :
In order for Remotely Piloted Aircraft Systems (RPAS) to coexist seamlessly with manned aircraft in non-segregated airspace, enhanced navigational capabilities are essential to meet the Required Navigational Performance (RNP) levels in all flight phases. A Multi-Sensor Data Fusion (MSDF) framework is adopted to improve the navigation capabilities of an integrated Navigation and Guidance System (NGS) designed for small-sized RPAS. The MSDF architecture includes low-cost and low weight/volume navigation sensors suitable for various classes of RPAS. The selected sensors include Global Navigation Satellite Systems (GNSS), Micro-Electro-Mechanical System (MEMS) based Inertial Measurement Unit (IMU) and Vision Based Sensors (VBS). A loosely integrated navigation architecture is presented where an Unscented Kalman Filter (UKF) is used to combine the navigation sensor measurements. The presented UKF based VBS-INS-GNSS-ADM (U-VIGA) architecture is an evolution of previous research performed on Extended Kalman Filter (EKF) based VBS-INS-GNSS (E-VIGA) systems. An Aircraft Dynamics Model (ADM) is adopted as a virtual sensor and acts as a knowledge-based module providing additional position and attitude information, which is pre-processed by an additional/local UKF. The E-VIGA and U-VIGA performances are evaluated in a small RPAS integration scheme (i.e., AEROSONDE RPAS platform) by exploring a representative cross-section of this RPAS operational flight envelope. The position and attitude accuracy comparison shows that the E-VIGA and U-VIGA systems fulfill the relevant RNP criteria, including precision approach in CAT-II. A novel Human Machine Interface (HMI) architecture is also presented, whose design takes into consideration the coordination tasks of multiple human operators. In addition, the interface scheme incorporates the human operator as an integral part of the control loop providing a higher level of situational awareness.
Keywords :
Kalman filters; aircraft control; aircraft navigation; autonomous aerial vehicles; mobile robots; nonlinear filters; robot vision; sensor fusion; GNSS; Global Navigation Satellite Systems; IMU; MEMS; MSDF framework; NGS; RPAS; UKF; VBS; inertial measurement unit; microelectromechanical system; multisensor data fusion technique; navigation and guidance system; remotely piloted aircraft system; unscented Kalman filter; vision based sensor; Aircraft; Aircraft navigation; Covariance matrices; Data integration; Mathematical model; Sensor systems; Aircraft Dynamics Model; Human Machine Interface; Low-cost sensors; Multi-sensor Data Fusion; Navigation and Guidance System; Remotely Piloted Aircraft Systems; Unscented Kalman Filter;
Conference_Titel :
Unmanned Aircraft Systems (ICUAS), 2015 International Conference on
Conference_Location :
Denver, CO
Print_ISBN :
978-1-4799-6009-5
DOI :
10.1109/ICUAS.2015.7152354