Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/427799
Title: Mid Air Collision Avoidance of Unmanned Aerial Vehicles
Researcher: Tony, Lima Agnel
Guide(s): Ghose, Debasish
Keywords: Engineering
Engineering Aerospace
Engineering and Technology
University: Indian Institute of Science Bangalore
Completed Date: 2021
Abstract: Autonomy is an essential feature of any robotic system. Aerial robots, commonly known as Unmanned Aerial Vehicles (UAVs), are being integrated into airspace and various trials towards achieving higher levels of autonomy are in progress. When multiple UAVs share the same airspace, safety from inter-UAV conflict is of utmost importance. Collision avoidance is an unavoidable feature of any UAV, and diverse methods addressing this problem are available in the literature. This thesis presents avoidance maps, a collision avoidance algorithm for fixed-wing UAVs. Avoidance of fixed-wing UAVs is challenging because of their inability to hover in contrast to their rotary-wing counterpart. Further, physical constraints like minimum turn radius make the process less flexible. The proposed avoidance map partitions the control input space of the UAVs into those leading to collision (red region) and avoidance (green region). Here, the control input used is constant lateral acceleration. Various versions of this are developed, which improves its computational cost. The algorithm could be implemented for cooperative, non-cooperative, and multiple UAVs and is demonstrated by suitable examples. In the next part of this thesis, precision UAV collision avoidance is discussed. This method is characterized by a gradual reduction of applied lateral acceleration during the avoidance process. Precision-control based avoidance optimizes the energy expenditure of the UAVs. The UAVs get away from their initial course while maneuvering. They are brought back to the initial direction of motion using Dubins curves, which joins two points via the shortest distance. The return to the course is achieved by Dubins path, where the necessary maneuvers are chosen from the avoidance map. An avoidance map can be used for realistic systems also. This utility is demonstrated by simulations using guidance models and six-degree-of-freedom UAV models. The avoidance map is further extended to few versions in the subsequent chapter. A time-graded version is...
Pagination: 
URI: http://hdl.handle.net/10603/427799
Appears in Departments:Aerospace Engineering

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01_title.pdfAttached File133.38 kBAdobe PDFView/Open
02_prelim pages.pdf311.91 kBAdobe PDFView/Open
02_table of contents.pdf64.84 kBAdobe PDFView/Open
04_abstract.pdf85.3 kBAdobe PDFView/Open
05_chapter 1.pdf228.62 kBAdobe PDFView/Open
06_chapter 2.pdf1.46 MBAdobe PDFView/Open
07__chapter 3.pdf1.42 MBAdobe PDFView/Open
08_chapter 4.pdf3.49 MBAdobe PDFView/Open
09_chapter 5.pdf1.9 MBAdobe PDFView/Open
10_chapter 6.pdf2.2 MBAdobe PDFView/Open
11_annexure.pdf356.59 kBAdobe PDFView/Open
80_recommendation.pdf184.52 kBAdobe PDFView/Open
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