Design of Variable Damping INS for Ships Based on the Variation of Reference Velocity Error

Author:

Liu Chuang1ORCID,Wu Qiuping1ORCID,Hu Peida1ORCID,Zhang Rong1ORCID

Affiliation:

1. Department of Precision Instrument, Tsinghua University, Beijing 100084, China

Abstract

Schuler oscillation damping is one of the key technologies to improve the long-term precision of inertial navigation systems (INSs). Generally, a ship introduces the reference velocity to work on the external horizontal damping status to avoid the effects caused by maneuvers. However, the navigation accuracy is sensitive to the reference velocity error which will be affected by sea conditions and the ship’s maneuver. It is necessary to adjust the damping status dynamically as the change of the reference velocity error to ensure the accuracy and stability of INS. To address this problem, a novel variable damping system based on the variation of the reference velocity error is designed in this paper. First of all, this proposed method switched the damping status according to the variation of the reference velocity error in a certain period of time based on the principle of window detection. In addition, this paper designed a fuzzy controller to avoid the overshoot caused by the frequent switching of the damping status. What is more, a method of overshoot suppression was applied in this system. Simulation experiments were conducted to validate the theoretical analysis and the effectiveness of this method. Compared with the undamping system, constant damping system, and traditional variable damping system, the simulation results verified that the designed variable damping system can attenuate the system error caused by reference velocity error most effectively, thus improving the navigation accuracy of INS.

Funder

National Natural Science Foundation of China

Publisher

Hindawi Limited

Subject

Electrical and Electronic Engineering,Instrumentation,Control and Systems Engineering

Reference33 articles.

1. Inertial navigation: from gimbaled platforms to strapdown sensors;D. A. Tazartes;IEEE Transactions on Aerospace and Electronic Systems,2011

2. Strapdown Inertial Navigation Technology

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