Class of vector fields for path following guidance (Record no. 432671)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 04334nam a22002177a 4500 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 240910b |||||||| |||| 00| 0 eng d |
| 082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | 629.8 |
| Item number | SHI |
| 100 ## - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Shivam, Amit |
| 245 ## - TITLE STATEMENT | |
| Title | Class of vector fields for path following guidance |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) | |
| Place of publication, distribution, etc | Bangalore : |
| Name of publisher, distributor, etc | Indian Institute of Science, |
| Date of publication, distribution, etc | 2024. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | xxii, 112 p. : |
| Other physical details | col. ill. |
| Accompanying material | e- Thesis. |
| Size of unit | 7.124 Mb. |
| 500 ## - GENERAL NOTE | |
| General note | Includes bibliography. |
| 502 ## - DISSERTATION NOTE | |
| Dissertation note | PhD;2024;Aerospace Engineering. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc | With rapidly evolving application scenarios, Unmanned Aerial Vehicles (UAVs) are often desired to autonomously follow predefined paths. Prospective path following guidance methods should cater to the dynamic capability of the UAV, curvature variation along the path, and provide accurate performance while utilizing, preferably, a computationally inexpensive guidance logic. This thesis presents a class of vector fields addressing a variety of path following guidance problems. The first part of the thesis considers constant curvature paths, namely, straight lines and circular orbits. The key idea is to generate the commanded UAV course angle as a vector field based on the instantaneous UAV position. The vector field logic uses an arcsine shaping function based on the UAV position with respect to the desired path. A stability analysis guarantees asymptotic convergence of the UAV position error to zero. A detailed comparative study with a popular approach demonstrates that the proposed method significantly reduces the maximum curvature and the total control effort along the guided trajectory. Numerical simulation studies consider a second-order course hold autopilot, first-order airspeed control and different UAV initial conditions to demonstrate the effectiveness of the proposed guidance method. The second part of the thesis considers scenarios wherein the path exhibits variation in its curvature. The first case therein considers an elliptic path following scenario, and a course angle guidance command is proposed which encompasses path convergent and path tangential components. The path convergent term is deduced using an arcsine shaping function of the UAV position error with respect to the path, while the tangential component is obtained using the slope information of the path. The second path following case considers paths described explicitly as y = f(x). Therein, again the course angle guidance command comprises path-tracking and path-attracting elements. Subject to the proposed guidance methods, asymptotically converging behavior of the UAV position error is deduced using Lyapunov stability theory. Extensive simulation studies are carried out with several UAV initial positions for following elliptic, sinusoidal and parabolic paths. Next, the thesis introduces rectangular boundary surveillance guidance using Lam\'e curve paths. Geometric properties of the Lam\'e curve paths are analyzed, and an efficient Lam\'e curve path based circumscriptions of a rectangular boundary is proposed. Considering a given UAV maximum turn rate, a comparative analysis highlights that the proposed Lam\'e curve path offers significantly reduced path length in circumscribing rectangular boundaries as compared to widely used elliptic circumscription. Further, a vector field guidance method is introduced to follow the Lam\'e curve path and its stability properties are established. Numerical simulation studies include sample scenarios with several UAV initial conditions and comparative studies with different rectangular dimensions.\par Using an indoor motion capture facility and a quadrotor UAV platform, the last part of the thesis presents experimental validation studies of the proposed guidance methods. Flight trials consider a variety of constant and variable curvature paths, and demonstrate the effectiveness of the proposed guidance methods. Overall, the proposed guidance methods present simple, analytic, and easily computable path-following logic that utilize only the UAV position information. Deterministic performance guarantees and extensive validation studies further add to the merit of the proposed guidance solutions. |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | Lam curve |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | Guidance |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | Path planning |
| 700 ## - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Advised by Ratnoo, Ashwini. |
| 856 ## - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | https://etd.iisc.ac.in/handle/2005/6616 |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | Thesis |
No items available.
