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Aircraft distribution type network all-physical ground simulation device and method

A ground simulation and aircraft technology, applied in the field of measurement, can solve the problems that cannot be constructed with a distributed full-physics simulation platform, and is not suitable for full-physics simulation, and achieves the effect of easy implementation, simple design principle and low cost

Active Publication Date: 2013-12-18
HARBIN INST OF TECH
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  • Abstract
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  • Application Information

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Problems solved by technology

[0006] China's invention patent (application number 201010544722.5) titled "Distributed Simulation Platform for Satellite Dynamics and Control" builds a distributed digital simulation platform for satellite dynamics and control to achieve "flexible" design of satellite control systems for different tasks, but the patent It is not suitable for full-physics simulation, and cannot be used for the construction of distributed full-physics simulation platform

Method used

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  • Aircraft distribution type network all-physical ground simulation device and method

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Effect test

Embodiment 1

[0015] to combine figure 1 , a distributed networked full-physics ground simulation device for an aircraft, which is composed of a dynamic drive subsystem 1, a kinematics simulation subsystem 2, a remote control computer subsystem 3, and an aircraft measurement load subsystem 4, and the aircraft measurement load carrier System 4 is installed on kinematics simulation subsystem 2, while dynamics driving subsystem 1, kinematics simulation subsystem 2 and remote control computer subsystem 3 are distributed, that is, they may be distributed in different areas for Working, and connected to each other through the network to realize the transmission of instructions and data.

[0016] The aircraft measurement load subsystem 4 can install measurement loads actually used by aircraft such as gyroscopes, inertial groups, or microwave radars or use simulation equipment thereof according to actual requirements of test simulation.

[0017] Described a kind of aircraft distributed networked f...

Embodiment 2

[0024] to combine figure 1 , the dynamic drive subsystem 1 is mainly composed of a three-axis air bearing platform 5, and an attitude measurement device 6, a motion actuator 7, a quality characteristic adjustment mechanism 8, etc., which can realize the measurement of the attitude of the air bearing platform, air flotation The attitude control of the platform and the adjustment of mass characteristics, and the attitude information of the air bearing platform are sent to the kinematics simulation subsystem 2 through the network. Among them, the attitude measurement device can use the Chinese invention patent "three-axis air bearing platform high-precision attitude angle measurement method and its device" (application number: 201110249979.2) or "three-axis air bearing platform high-precision attitude angle and angular velocity measurement device" (application number : 201310134631.8) the method used. The motion actuator of the air bearing table can use devices such as reaction ...

Embodiment 3

[0026] to combine figure 1 , the kinematics simulation subsystem 2 is mainly composed of a three-axis electric turntable, the aircraft measurement load subsystem 4 is installed on the turntable, and the three-axis electric turntable receives the attitude information of the dynamic drive subsystem 1 through the network and controls the three-axis turntable To achieve high-precision reproduction of the attitude, the used aircraft measurement load subsystem 4 transmits the measured attitude information to the remote control computer through the network.

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Abstract

The invention provides an aircraft distribution type network all-physical ground simulation device. The device comprises a dynamics driving sub-system, a kinematic simulation sub-system, a remote control computer sub-system and an aircraft measurement loading sub-system. The aircraft measurement load sub-system is arranged on the kinematic simulation sub-system, the dynamic driving sub-system, the kinematic simulation sub-system and the remote control computer sub-system are arranged in a distribution mode, the dynamics driving sub-system comprises a triaxial air floating platform, a posture measurement device, a movement actuating mechanism and a quality characteristic adjusting mechanism. The invention further provides an aircraft distribution type network all-physical ground simulation method, an integral system is composed of simulation devices distributed at different locations, and the simulation devices are combined according to practical requirements. The system is simple in design principle, easy to achieve, low in cost and capable of achieving close-loop tests of an aircraft sensor and a control algorithm, and kinetic data provided by the triaxial air floating platform are real control results.

Description

technical field [0001] The invention relates to measurement technology, in particular to a distributed networked full physical ground simulation device and method for an aircraft. Background technique [0002] Once the space vehicle is launched, it will be difficult to maintain, and its special operating environment makes the ground simulation test particularly important. At present, the space vehicle ground simulation is mainly divided into three categories: (1) mathematical / computer software simulation; (2) semi-physical simulation; (3) Full physical simulation. One of the most effective and convincing is the full physical simulation test. The three-axis air bearing table in its core equipment room relies on the air film formed between the air bearing and the bearing seat by compressed air to make the simulated table body float, so as to realize the relative motion condition of approximately frictionless, so as to simulate space vehicles such as satellites A mechanical e...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02
Inventor 夏红伟李莉马广程王常虹宋效正王艳敏任家栋
Owner HARBIN INST OF TECH
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