Vision/INS Integrated Navigation System for Poor Vision Navigation Environments

被引:8
|
作者
Kim, Youngsun [1 ]
Hwang, Dong-Hwan [2 ]
机构
[1] Korea Aerosp Res Inst, Payload Elect Team, Daejon 34133, South Korea
[2] Chungnam Natl Univ, Dept Elect Engn, Daejon 34134, South Korea
关键词
vision navigation system; inertial navigation system; integrated navigation; focal plane measurements; landmark;
D O I
10.3390/s16101672
中图分类号
O65 [分析化学];
学科分类号
070302 ; 081704 ;
摘要
In order to improve the performance of an inertial navigation system, many aiding sensors can be used. Among these aiding sensors, a vision sensor is of particular note due to its benefits in terms of weight, cost, and power consumption. This paper proposes an inertial and vision integrated navigation method for poor vision navigation environments. The proposed method uses focal plane measurements of landmarks in order to provide position, velocity and attitude outputs even when the number of landmarks on the focal plane is not enough for navigation. In order to verify the proposed method, computer simulations and van tests are carried out. The results show that the proposed method gives accurate and reliable position, velocity and attitude outputs when the number of landmarks is insufficient.
引用
收藏
页数:14
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