UAV flight simulation system and safety test system
A technology for flight simulation and safety testing, applied in the field of UAVs, which can solve problems such as the inability to fully understand the flight safety of UAVs
Active Publication Date: 2018-08-21
CHINA ELECTRONICS PROD RELIABILITY & ENVIRONMENTAL TESTING RES INST
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Problems solved by technology
[0004] Based on this, it is necessary to provide a UAV flight simulation system for the problem that traditional UAV experiments cannot fully understand the safety of UAV flight
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[0024] In order to facilitate the understanding of the present invention, the present invention will be described more fully below with reference to the associated drawings. Preferred embodiments of the invention are shown in the accompanying drawings. However, the present invention can be embodied in many different forms and is not limited to the embodiments described herein. On the contrary, these embodiments are provided to make the understanding of the disclosure of the present invention more thorough and comprehensive.
[0025] It should be noted that when an element is referred to as being “fixed” to another element, it can be directly on the other element or there can also be an intervening element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or intervening elements may also be present.
[0026] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as...
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The invention relates to a UAV flight simulation system and a safety test system. The simulation system comprises: a translation mechanism; a posture simulation mechanism which reciprocally translatesunder the drive of the translation mechanism; the posture simulation mechanism comprises a bottom plate, a posture adjustment component and a carrier plate. The bottom plate is disposed on the translation mechanism; the carrier plate is disposed at a distance from the side of the bottom plate away from the translation mechanism; the posture adjustment component is disposed between the bottom plate and the carrier plate; the posture adjustment component drives the carrier plate to swing relative to the bottom plate. The posture adjustment component makes the UAV change different postures, andthe translation mechanism drives the posture simulation mechanism to reciprocate and translate to simulate a dynamic process of the UAV, and finally the real-time posture of the carrier plate is acquired through a posture sensor, and dynamic performance of the UAV is acquired.
Description
technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle flight simulation system and a safety test system. Background technique [0002] With the rapid development of drone technology and the increasing market demand, low-altitude, low-cost civilian drones are increasingly used in aerial photography, agriculture, forestry, security, power and other industries. Due to the low technical threshold for civil drones, the huge market prospects, and the lack of unified manufacturing requirements, not only some aviation-related supporting companies are vigorously developing drones, but many aircraft model companies can also complete the assembly of drones by purchasing parts. Effective methods and technologies are used to test and evaluate UAV products, which leads to frequent occurrence of UAV safety accidents. Therefore, it is necessary to evaluate the safety performance of the UAV flight process...
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IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 杨剑锋李小兵王远航黄创绵董成举蔡茗茜刘文威丁小健潘广泽黄强
Owner CHINA ELECTRONICS PROD RELIABILITY & ENVIRONMENTAL TESTING RES INST