Research Article

An Operational Safety Evaluation Method for Manned Transport Aircraft and Large UAV in Mixed Airspace

Table 3

Comparison of experimental results based on the two algorithms.

Experimental design sequence numberTypes of experimental resultsModel of GBAS (within 15 kilometers; outside 15 kilometers)PTD-MI

The first caseThe total deviation M, km>2.588; >3.844>3.116
Total number of aircraft (A + B), frame/km31.281 × 10−3; 0.982 × 10−31.203 × 10−3
The second caseThe total deviation M, km>3.602; >5.013>4.214
Total number of aircraft (A + B), frame/km30.962 × 10−3; 0.615 × 10−30.895 × 10−3
The third caseThe total deviation M, km>3.116; >4.607>3.762
Total number of aircraft (A + B), frame/km31.138 × 10−3; 0.807 × 10−31.054 × 10−3