Ground risk evaluation method in unmanned aerial vehicle operation safety risk evaluation
A technology for operating safety risks and UAVs, which is applied in the field of ground risk assessment in UAV operation safety risk assessment, can solve the problems of lack of UAV operation safety risk assessment models and methods, and achieve rich means of information acquisition , wide coverage and comprehensive effects
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Embodiment 1
[0136] Embodiment 1: The ground risk assessment and analysis of Talon UAV colliding with general aviation aircraft in the air:
[0137] According to the steps of the method of the present invention, the relevant parameter information and environmental parameters of the Talon UAV are first obtained, as shown in Table 3.
[0138] Table 3 UAV simulation parameter table
[0139]
[0140] Assuming that the cause of UAV system failure is air collision, the calculation of air collision probability needs to know the parameters of UAV and other aircraft, including the air traffic density in the operating area. Since the parameters of other aircraft and air density are unknown, so at this time Reasonable assumptions based on the literature are required. Relevant data can also be obtained by monitoring air traffic in the region. The monitoring method can be to record the distribution of other aircraft in the airspace multiple times, divide the number of aircraft in the airspace by t...
Embodiment 2
[0151] Embodiment 2: Assessment and analysis of the ground risk when the Talon UAV system fails:
[0152] According to the steps of the method of the present invention, the relevant parameter information and environmental parameters of the Talon UAV are first obtained, which is the same as that in Embodiment 1.
[0153] Assuming that the cause of UAV system failure is system failure, the possibility of UAV ballistic descent and gliding descent due to system failure is estimated according to relevant information and literature, as shown in Table 5.
[0154] Table 5 System Failure Probability
[0155] ballistic drop gliding descent Failure rate (per flight hour) 1 / 200 1 / 200
[0156] Also due to the lack of experimental results in this regard, three situations are assumed in the simulation: ballistic descent, gliding descent, and a combination of the two methods of descent (assuming that after mid-air collisions, 70% may descend by ballistic descent, and...
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