Vision-based fixed point robust control method for airship

A robust control and airship technology, applied in the field of airship flight control, can solve problems such as airship position and attitude estimation

Inactive Publication Date: 2011-09-21
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
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  • Application Information

AI Technical Summary

Problems solved by technology

Two key issues that need to be solved are: 1. Estimation of airship position and attitude
However,

Method used

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  • Vision-based fixed point robust control method for airship
  • Vision-based fixed point robust control method for airship
  • Vision-based fixed point robust control method for airship

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Embodiment Construction

[0028] figure 1It is the overall control block diagram of the airship. Its system is divided into the ship-borne part and the ground control station part. The specific working principle is: firstly, the ship-borne camera takes a sequence of images of ground markers, transmits them through the ship-mounted antenna, and receives them from the ground station. The device receives and transmits to the ground station control computer. The ground computer quickly processes it to obtain the features of the markers, and completes the estimation of the attitude and position of the airship through these features. Then the airship's attitude and position estimates are transmitted by the transmitting antenna on the ground, received by the receiving equipment on the airship, and transmitted to the on-board computer, which completes the proportional combination of the estimated value and the signal measured by the on-board sensor The control feedback signal is formed by merging in the same ...

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Abstract

The invention relates to a vision-based fixed point robust control method for an airship, which comprises the following steps of: defining a ground coordinate system, an aircraft body coordinate system, a speed coordinate system and an image coordinate system and determining a mounting mode of an airborne camera on the basis; extracting an attitude angle of the airship according to the projectivegeometry principle; obtaining a nonlinear equations set containing the attribute and the position of the airship according to a binocular vision parallax principle; and substituting the attitude angle obtained in the second step into the nonlinear equations set to obtain the position of the airship. By adopting the robust self-adaptive fixed point control scheme for designing the airship by adopting a Backstepping method as well as a Backstepping control scheme provided by analyzing and proving, the bounded stability of a closed loop system can be effectively ensured; and the attitude angle and the position information obtained on the basis of an image are combined with control so that the closed loop control is realized. In the vision-based fixed point robust control method, the positionand attribute information extracted by using a position and attribute estimation algorithm is loaded into an airship fixed point control technology to realize the vision-based control to the fixed points of the airship.

Description

technical field [0001] The invention belongs to the field of airship flight control, in particular to a vision-based fixed-point robust control method for an airship. Background technique [0002] At present, airships have attracted people's attention and are widely used in various fields such as freight, advertising, surveillance, and military missions. An airship is a maneuverable aircraft that is lighter than air. It floats in the air by the buoyancy of the light gas enclosed by the air bag, and can fly in the air by the power of the engine. As a kind of aircraft, the biggest advantage of the airship is that it has an unparalleled time in the air, and its air time can be calculated in days. At the same time, the airship can also fly stably in the air quietly, which also has important military applications. At present, military airships generally use helium to maintain buoyancy, so they can complete lifting and flight quietly and smoothly, which is crucial for carrying m...

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Application Information

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IPC IPC(8): B64B1/00G05D1/00
Inventor 陈谋江驹姜长生尹卫平
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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