基于大地坐标系的IMM航空器短期航迹外推

doi:10.12305/j.issn.1001-506X.2022.07.26

Abstract

Abstract:

Aiming at the aircraft in route flight phase, the geodetic coordinate system is used to represent the position of the aircraft after comparing the advantages and disadvantages of the space rectangular coordinate system and the geodetic coordinate system. Based on the geodetic coordinate system, the motion of the aircraft is decoupled into independent motion in three directions, and the sub models in each direction are established respectively. The interacting multiple model (IMM) algorithm is used to track the trajectory of the aircraft. The simulation results show that the IMM algorithm based on geodetic coordinate system has good tracking performance for aircraft. According to the aircraft terminal state and the probability distribution of each sub-model, the aircraft's trajectory is short-term extrapolated. The track extrapolation performance of the IMM algorithm based on the geodetic coordinate system is better than that of the IMM algorithm based on the space rectangular coordinate system.

Key words: air traffic management, trajectory tracking, short-term track extrapolation, interacting multiple model (IMM)

CLC Number:

Xinmin TANG, Pengcheng ZHENG. IMM aircraft short-term track extrapolation based on geodetic coordinate system[J]. Systems Engineering and Electronics, 2022, 44(7): 2293-2301.

Figures/Tables 12

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序号	描述
1	经度方向的匀角速度运动模型 (constant angular velocity of L, CAVL)
2	经度方向的“当前”运动模型 (current statistical of L, CSL)
3	纬度方向的匀角速度运动模型 (constant angular velocity of B, CAVB)
4	纬度方向的“当前”运动模型 (current statistical of B, CSB)
5	高速方向上的零速运动模型 (constant height, CH)
6	高度方向的“当前”运动模型 (current statistical of H, CSH)

运动状态	模型集组合
在大圆航线平飞	CAVL+CAVB+CSL+CSB+CH
沿大圆航线升降	CAVL+CAVB+CSL+CSB+CSH
沿等角航线平飞	CAVL+CAVB+CSL+CSB+CH
沿等角航线升降	CAVL+CAVB+CSL+CSB+CSH
保持高度转弯	CAVL+CAVB+CSL+CSB+CH
升降过程中转弯	CAVL+CAVB+CSL+CSB+CSH

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IMM aircraft short-term track extrapolation based on geodetic coordinate system

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