title: Vision/INS Integrated Navigation System for Poor Vision Navigation Environments.
abstract: 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.
authors.affiliation: Payload Electronics Team, Korea Aerospace Research Institute, Daejon 34133, Korea. yskim1203@kari.re.kr.
authors.forename: Youngsun
authors.initials: Y
authors.lastname: Kim
authors.affiliation: Department of Electronics Engineering, Chungnam National University, Daejon 34134, Korea. dhhwang@cnu.ac.kr.
authors.forename: Dong-Hwan
authors.initials: DH
authors.lastname: Hwang
keywords: focal plane measurements; inertial navigation system; integrated navigation; landmark; vision navigation system