4.5 Article

Concept and Feasibility Evaluation of Distributed Sensor-Based Measurement Systems Using Formation Flying Multicopters

期刊

ATMOSPHERE
卷 12, 期 7, 页码 -

出版社

MDPI
DOI: 10.3390/atmos12070874

关键词

multicopters; formation flying; optical atmospheric measurement; distributed sensor; gimbal stabilization system; sliding mode control; disturbance modeling

资金

  1. Technische Universitat Braunschweig [12plus6]
  2. German Research Foundation - German Research Foundation
  3. Open Access Publication Funds of Technische Universitat Braunschweig

向作者/读者索取更多资源

This paper proposes a new concept of using tandem flying multicopters as a distributed sensor platform for atmospheric measurements. The key challenges include relative position estimation and control in wind-perturbed outdoor environments, and precise alignment of payloads. Experimental data is used to evaluate the performance of the sliding mode controller and gimbal stabilization system in achieving achievable control accuracies of the relative position and attitude of subsystems in the proposed concept.
Unmanned aerial vehicles (UAVs) have been used for increasing research applications in atmospheric measurements. However, most current solutions for these applications are based on a single UAV with limited payload capacity. In order to address the limitations of the single UAV-based approach, this paper proposes a new concept of measurements using tandem flying multicopters as a distributed sensor platform. Key challenges of the proposed concept are identified including the relative position estimation and control in wind-perturbed outdoor environment and the precise alignment of payloads. In the proposed concept, sliding mode control is chosen as the relative position controller and a gimbal stabilization system is introduced to achieve fine payload alignment. The characterization of the position estimation sensors (including global navigation satellite system and real-time kinematics) and flight controller is carried out using different UAVs (a DJI Matrice M600 Pro Hexacopter and Tarot X4 frame based Quadcopter) under different wind levels. Based on the experimental data, the performance of the sliding mode controller and the performance of the gimbal stabilization system are evaluated in a hardware-in-the-loop simulation environment (called ELISSA). Preliminary achievable control accuracies of the relative position and attitude of subsystems in the proposed concept are estimated based on experimental results.

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