2016
DOI: 10.1016/j.ast.2016.09.002
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A low-cost and high performance navigation system for small RPAS applications

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Cited by 27 publications
(11 citation statements)
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“…The performance of VBN sensors is affected by low visibility conditions which could be due to night/low light conditions, smoke, fog, precipitation as well as presence of transparent or opaque objects [ 70 ]. An ADM virtual sensor is dependent on the aircraft’s physical sensors and is based on the assumption of the aircraft being a rigid body with a constant and static mass distribution [ 71 ]. An integration of sensor data achieved through Multi-Sensor Data Fusion algorithms can lead to an improved positioning solution for air and ground platforms.…”
Section: Integration Of Acoustic Sensors In Multi-sensor Navigatiomentioning
confidence: 99%
“…The performance of VBN sensors is affected by low visibility conditions which could be due to night/low light conditions, smoke, fog, precipitation as well as presence of transparent or opaque objects [ 70 ]. An ADM virtual sensor is dependent on the aircraft’s physical sensors and is based on the assumption of the aircraft being a rigid body with a constant and static mass distribution [ 71 ]. An integration of sensor data achieved through Multi-Sensor Data Fusion algorithms can lead to an improved positioning solution for air and ground platforms.…”
Section: Integration Of Acoustic Sensors In Multi-sensor Navigatiomentioning
confidence: 99%
“…The European Commission's Directorate General for Mobility and Transport (DG MOVE), the European Defence Agency (EDA), the European Aviation Safety Agency (EASA), and the Single European Sky Air Traffic Management (ATM) Research (SESAR) Joint Undertaking (SJU) are also stepping up the efforts to safely accommodate UAS into the European aviation and ATM system [6]. In parallel with these government and industry-led initiatives, the aerospace research community has been continuously working on several challenges of integrating UAS into non-segregated airspaces including separation thresholds and methods for small UAS [7,8], UAS encounter modelling and collision avoidance [9][10][11], 3D obstacle avoidance strategies for UAS [12][13][14][15] dynamic model augmentation [16], Global Navigation Satellite Systems (GNSS) integrity augmentation for UAS [17], surveillance sensor integration in the UAS platform [18,19] and well-clear boundary models for UAS DAA [20][21][22][23][24].…”
Section: Introductionmentioning
confidence: 99%
“…Figure 1 describes the above discrete Kalman filter algorithm, we can see from the figure Kalman filter which has two calculation loops [19,20]. Among them, the gain calculation circuit is an independent calculation circuit, and the filter calculation circuit depends on the gain calculation circuit.…”
Section: Combined Positioning Path Planningmentioning
confidence: 99%