Unmanned helicopter ground testing console and application method thereof

An unmanned helicopter and debugging platform technology, applied in the field of ground adjustment, can solve the problems of high control technology requirements, low safety in the debugging process, and difficulty in ensuring the accuracy of the debugging results, so as to reduce storage space, improve debugging work efficiency, The effect of improving the efficiency of debugging work

Active Publication Date: 2015-04-08
NAVAL AERONAUTICAL & ASTRONAUTICAL UNIV PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is to provide a ground debugging platform for unmanned helicopters, which solves the problem that the existing unmanned helicopter stabilization equipment PID para

Method used

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  • Unmanned helicopter ground testing console and application method thereof
  • Unmanned helicopter ground testing console and application method thereof
  • Unmanned helicopter ground testing console and application method thereof

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Experimental program
Comparison scheme
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Embodiment 1

[0034] For general unmanned helicopters (unless the landing gear of the unmanned helicopter is short, the data acquisition module cannot be installed under the landing gear), such as figure 1 The structure of the unmanned helicopter ground debugging platform shown.

[0035] The unmanned helicopter ground debugging platform includes: an unmanned helicopter installation plate 1, a data acquisition module 2, a support rod 4 and a base 5.

[0036] The data acquisition module 2 is installed on the upper surface of the unmanned helicopter mounting plate 1 by bolts, and a vibration damping pad is installed between the data acquisition module 2 and the unmanned helicopter mounting plate 1, and the installation center of the data acquisition module 2 is installed with the unmanned helicopter. The center of the disk 1 coincides; the upper end of the support rod 4 and the unmanned helicopter installation disk 1 are connected through a ball bearing and a bearing seat, and the unmanned hel...

Embodiment 2

[0041] The structure of this embodiment is to replace the ball bearing and the bearing block in the structure of the unmanned helicopter ground debugging platform mentioned in embodiment 1 with a universal joint. In addition, the connection between the upper end of the support rod and the mounting plate of the unmanned helicopter can also be connected through other forms of universal rotation mechanism, as long as the universal rotation mechanism can make the mounting plate 1 of the unmanned helicopter rotate around the universal direction. The mechanism can rotate freely, including pitch, yaw and roll, and its coupled motion.

Embodiment 3

[0043] The unmanned helicopter ground debugging platform structure mentioned in this embodiment is mainly used for the debugging of unmanned helicopters with short landing gear (the data acquisition module cannot be installed under the landing gear), and its structure is as follows Figure 5 shown.

[0044] The structure of the present embodiment is on the basis of the unmanned helicopter ground debugging platform structure mentioned in embodiment 1, and the data acquisition module installation disk 3 is increased, and the data acquisition module installation disk 3 and the unmanned helicopter installation disk 1 are installed concentrically and parallelly, Studs are used to install between them, and other detachable connection methods such as bolts can also be used; the data acquisition module 2 is no longer installed on the upper surface of the unmanned helicopter mounting plate 1, but is installed on the data acquisition module. The upper surface of the disk 3, and the inst...

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Abstract

The invention relates to an unmanned helicopter ground testing console and an application method thereof. The testing console comprises an unmanned helicopter mounting disc, a data acquiring module, a support rod and a base; if an undercarriage is relatively short, an independent data acquiring module mounting disc is arranged between the unmanned helicopter mounting disc and the support rod. The support rod and the unmanned helicopter mounting disc/the data acquiring module mounting disc are connected by an universal rotating mechanism; and a removable hoop is arranged for keeping the mounting disc horizontal in the detaching of an unmanned helicopter. The testing console and the application method thereof are used for solving the problems of higher requirement of a PID parameter testing mode of traditional unmanned helicopter autostability equipment for the control skill of control staff, lower safety in the testing process and difficult guarantee of the precision degree of testing results. The testing console has such advantages as simple structure and convenience for use, disassembly, storage and carrying; and correspondingly, the application method is clear in process, is convenient for operation, and can largely shorten the PID parameter adjusting time.

Description

technical field [0001] The invention belongs to a ground debugging tool for an unmanned helicopter, and in particular relates to a ground debugging platform for an unmanned helicopter, and method steps for debugging an unmanned helicopter using the debugging platform. The debugging platform and debugging method are especially suitable for unmanned helicopters The ground debugging of manned helicopters specifically refers to the PID parameter debugging of unmanned helicopters equipped with stabilization equipment such as autopilots or gyroscopes. Background technique [0002] Whether in civilian or military fields, unmanned helicopters are increasingly used. In order to ensure safety and stability during flight, most unmanned helicopters are equipped with stabilization equipment such as autopilot or gyroscope. When the unmanned helicopter is newly installed or replaced with stabilization equipment, it is necessary to adjust the PID parameters of each channel of the unmanned ...

Claims

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Application Information

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IPC IPC(8): B64F1/00B64F5/00B64F5/60
Inventor 孟浩高永康小伟郭卫刚刘书岩程功王齐柳文林郁大照贾忠湖王秀霞
Owner NAVAL AERONAUTICAL & ASTRONAUTICAL UNIV PLA
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