Abstract:
By analyzing present state of the optoelectronic aid system of carrier landing, the component, configuration, technology principle and technology target of the optoelectronic aid landing system were presented. Combining with the existing technology, the key factors of location precision were analyzed deeply by swaying experiment and simulation. Under the condition of no-swing, pitching of 2and period of 20s, or rolling of 10and period of 15s, the location error of the optoelectronic aid landing system was provided when the distance between carrier aircraft and landing site was greater or less than 1 km.