运动学GPS着陆系统架构及飞行试验结果

Proceedings of IEEE National Telesystems Conference - NTC '94 Pub Date : 1994-05-26 DOI:10.1109/NTC.1994.316683

S. Cobb, C. Cohen, B. Parkinson

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引用次数: 0

摘要

仅给出摘要形式，如下。运动学GPS着陆系统(KGLS)利用差分GPS载波相位数据为着陆飞机导航。当飞机在接近过程中飞过“GPS标记信标”时，KGLS传感器使用信标数据来解决载波相位整数模糊。这种确定性方法提供了厘米级的精度和高可靠性。

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Kinematic GPS landing system architecture and flight test results

Summary form only given, as follows. The kinematic GPS landing system (KGLS) uses differential GPS carrier phase data to navigate landing aircraft. As the aircraft overflies a "GPS marker beacon" during its approach, the KGLS sensor uses beacon data to resolve the carrier phase integer ambiguity. This deterministic method provides centimeter-level accuracy and high reliability on every approach.<>

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Proceedings of IEEE National Telesystems Conference - NTC '94

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