| 摘要 |
The present invention refers to an aerial device of aerostatic-rotational hybrid sustainability, which is characterized in that the sustainability system combines four helices of vertical propulsion, two helices of longitudinal propulsion and a double structure of gas chambers. In addition, the system includes a mechanical structure that forms the main part of the body of the aerial device, which is formed by the combination of two simple basic pieces. The present invention has a flight control based on an on-board computer, which forms part of a node of a distributed system of communications. The on-board computer system includes the feedback of accelerometers of three axes, gyroscopes of three axes, inclinometer of three axes, vision sensors, GPS, barometer, and sensor of atmospheric pressure and temperature. |
