Swing inhibition method of local space elevator system in elliptical orbit

An elevator system and local space technology, applied in the aerospace field, can solve problems such as difficult prediction and control of the system, collision of the elevator system in local space, and difficulty in cleaning up, etc., and achieve good control effect, swing suppression, and avoid out-of-control effects

Active Publication Date: 2017-08-29
NORTHWESTERN POLYTECHNICAL UNIV
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Problems solved by technology

When the space elevator system runs on an elliptical orbit, the entire system will become difficult to predict and control due to the existence of chaotic mo

Method used

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  • Swing inhibition method of local space elevator system in elliptical orbit
  • Swing inhibition method of local space elevator system in elliptical orbit
  • Swing inhibition method of local space elevator system in elliptical orbit

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Embodiment Construction

[0035] The present invention is described in further detail below in conjunction with accompanying drawing:

[0036] see Figure 1-4 , the working body of the present invention is a local space elevator system composed of three spacecraft connected by two tethers. The length of the rope depends on the specific working conditions, generally speaking, it is about 10 kilometers. When all parts of the system are connected, the whole system can be regarded as a three-body space tether system. The invention establishes the model of the local space elevator system; proposes a control strategy aiming at the characteristics of the system; proposes an attitude control law aiming at the target system; and finally verifies the effectiveness of the method proposed by the invention with an example. The implementation of this invention mainly comprises following three steps:

[0037] Step 1. Local space elevator system dynamics model.

[0038] In the present invention, the rope is regard...

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Abstract

The present invention discloses a swing inhibition method of a local space elevator system in an elliptical orbit. A working body is a local space elevator system formed by three spacecrafts connected through two tethers. The lengths of the tethers are decided through a concrete condition, and are about 10 kilometers in a general way. When the connection of each portion of the system is completed, the whole system can be taken as a three-dimensional space tether system. A local space elevator system model is established, and a control strategy is provided aiming at the features of the system; an attitude control rule aiming at a target system is provided; and the experiment shows that: even if the system is operated on an orbit having a large eccentricity ratio, the swing inhibition method of local space elevator system in the elliptical orbit can avoid the occurrence of chaotic motion to cause out of control. The swing of the system can be effectively inhibited, and the configuration of the system can be maintained on the state required by the operation of the system. The size of the thrust required by control accords with the actual situation of the engineering, and the control effect is good.

Description

【Technical field】 [0001] The invention belongs to the field of aerospace technology, and relates to a swing suppression method for an elevator system in a local space in an elliptical orbit. 【Background technique】 [0002] With the development of space technology, space missions are becoming increasingly diverse and complex. Among many space systems, the local space elevator system is an on-orbit service technology with broad application prospects. The system can realize the transportation of goods and personnel between spacecraft with orbital gradient differences on the order of 10 kilometers to 100 kilometers, thereby avoiding the collision risk caused by the close approach and docking of space platforms, reducing fuel consumption, and greatly improving Safety of space platforms during missions. [0003] Most of the current local space elevator systems are three-body tether structures, which consist of three spacecraft and tethers connected between them. The material of...

Claims

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Application Information

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IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 朱战霞史格非袁建平
Owner NORTHWESTERN POLYTECHNICAL UNIV
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