题名: |
Effects of cable geometry and aircraft attitude on the accuracy of a magnetic leader cable system for aircraft guidance during rollout and turnoff |
作者: |
Bundick, W. T. |
关键词: |
geometry;attitude;magnet;cable;measurement;turn;lead;craft;ects;ader |
摘要: |
A theoretical analysis of a single wire magnetic leader cable system for aircraft rollout and turnoff guidance was performed to determine the errors produced by the leader cable installation geometry and aircraft attitude. It was found that errors in the measurement of lateral displacement from the cable are smaller than errors in the measurement of aircraft heading and that both errors are smallest at or near the cable. |
报告类型: |
科技报告 |