Affiliation:
1. University of China
2. Civil Aviation Flight University of China
Abstract
the unstable approach caused by the distortion of glideslope, endangers aircraft in the forms of over-pitching, stalling at low altitude, and exceeding the limitation of descent rate. Aiming at the issues above, this paper presents a glideslope distortion correction model based on the fusion of multi-navigation sensors. Model simulations have been done to prove the effectiveness of the model, and the results show that the correction model can enhance the stability of glideslope effectively.
Publisher
Trans Tech Publications, Ltd.