Name
Abstract | ||
|---|---|---|
This paper describes the process and challenges behind the design and development of a micro-gravity enabling aerial robot. The vehicle, designed to provide at minimum 4 seconds of micro-gravity at an accuracy of .001 gu0027s, is designed with suggestions and constraints from both academia and industry as well a regulatory agency. The feasibility of the flight mission is validated using a simulation environment, where models obtained from system identification of existing hardware are implemented to increase the fidelity of the simulation. The current development of a physical test bed is described. The vehicle employs both control and autonomy logic, which is developed in the Simulink environment and executed in a Pixhawk flight control board. |
Year | Venue | Field |
|---|---|---|
2016 | arXiv: Robotics | Change control board,Fidelity,Physical test,Simulation,Control engineering,Engineering,Robot,System identification |
DocType | Volume | Citations |
Journal | abs/1611.07650 | 0 |
PageRank | References | Authors |
0.34 | 0 | 5 |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Juan-Pablo Afman | 1 | 1 | 1.73 |
| John Franklin | 2 | 0 | 0.68 |
| Mark L. Mote | 3 | 0 | 0.68 |
| Thomas Gurriet | 4 | 7 | 3.26 |
| Eric Feron | 5 | 42 | 8.23 |