面向4D航迹运行的飞行冲突混杂系统理论监控方法

为实现未来大流量、高密度、小间隔条件下的空中交通管理,提出了一种避免飞行冲突的混杂控制系统结构。首先依据不同飞行状态下的航空器运动学方程建立被控对象模型,依据空中交通管制规则确定了禁止空中交通系统轨迹穿越的冲突超曲面,并通过设计监控器辨识潜在的冲突事件。然后基于管制员可采用的调配手段设计飞行冲突离散控制器,根据离散冲突事件向量确定可行的离散解脱策略,并在允许解脱时间段内且系统超曲面函数值的差分为负的前提下计算连续操纵输入量。案例研究表明,混杂系统理论模型能对潜在冲突进行实时探测和解脱,保证空中交通系统处于可达集的安全子集中。

4D Trajectory Based Operation Flight Conflict Supervisory Control Based on Hybrid System Theory

To resolve the problem of future air traffic management under great traffic flow, high density, and small separation condition, a hybrid control system structure for flight confliction supervisory control is proposed.Firstly, a set of kinematic equations for the aircraft are proposed according to different flight stages. The confliction hyper-surfaces are defined based on air traffic control rules to forbidden the trajectory of the system composed by multiple aircrafts to cross it, and the crossing events can be recognized by a designed supervisor. In addition, the flight confliction discrete controller is designed according to resolutions available for air traffic controller to decide which control input should be applied. The continuous control input vector is derived under the condition that the difference value of confliction hyper-surfaces keeps negative in a resolution period, which keeps the air traffic system in the safe space. Case study proves that the method based on hybrid system theory can detect potential conflictions and resolve them in advance.