THAAD增程型拦截弹预测制导方法

张荣升; 陈万春

doi:10.13700/j.bh.1001-5965.2018.0619

THAAD增程型拦截弹预测制导方法

doi: 10.13700/j.bh.1001-5965.2018.0619

张荣升,
陈万春^,

北京航空航天大学宇航学院, 北京 100083

详细信息

作者简介:
张荣升男, 硕士研究生。主要研究方向: 拦截弹预测制导

陈万春男, 博士, 教授, 博士生导师。主要研究方向: 导弹总体设计与仿真、导弹飞行动力学、制导与控制

通讯作者:
陈万春, E-mail: wanchun_chen@buaa.edu.cn

中图分类号: V448.232;TJ765.3
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- 文章访问数: 950
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- 被引次数: 0
出版历程
- 收稿日期: 2018-10-29
- 录用日期: 2019-01-11
- 网络出版日期: 2021-04-20

Predictive guidance method of THAAD-ER interceptor

ZHANG Rongsheng,
CHEN Wanchun^,

School of Astronautics, Beihang University, Beijing 100083, China

More Information

Corresponding author: CHEN Wanchun, E-mail: wanchun_chen@buaa.edu.cn

摘要

摘要:
根据公开资料对THAAD增程型拦截弹建模，针对大射程的特点规划了高抛弹道，生成标准弹道族。提出了迭代预测命中点法，利用解析方法计算剩余飞行时间，基于多项式拟合法寻找标准弹道，确定预测命中点，完成预测制导任务。将迭代预测命中点法与迭代飞行时间法进行对比，迭代预测命中点法初值选取容易，程序运行时间减少20%，制导过程中无需调用标准弹道文件，节省了计算机存储空间。通过改变射程、航路捷径对预测制导方法进行仿真验证，结果表明，拦截弹拦截射程可覆盖到600 km，并且能完成存在航路捷径时的拦截任务，平均脱靶量在200 m以内，应对气动不确定性的效果良好。
- THAAD增程型拦截弹 /
- 预测制导 /
- 标准弹道族 /
- 预测命中点 /
- 剩余飞行时间
Abstract:
Based on public information, the model of THAAD-ER interceptor was established. Aimed at longer range, the high throw trajectory was planned, and a bunch of standard trajectories were produced. Predicted impact point iterated method is proposed, which contains solving time-to-go with analytic solution, seeking out the expected standard trajectory with polynomial fitting, and ascertaining the predictive impact point, and finally predictive guidance completes. Comparison is taken between predicted impact point iterated method and flight time iterated method, and it is easy to choose initial value with predicted impact point iterated method, and the program runtime decreases by 20%; standard trajectory files are not necessary during guidance process, which can save storage space of the computer on the interceptor. Large amount of simulations were carried out with different range and course shortcut, and the results show that interception range of THAAD-ER interceptor can reach 600 km, and the interception task can be completed with average miss distance less than 200 m when course shortcut remains. It has a good response to aerodynamic uncertainty.
- THAAD-ER interceptor /
- predictive guidance /
- a bunch of standard trajectories /
- predicted impact point /
- time-to-go

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图 1 拦截弹主要尺寸

Figure 1. Main dimensions of interceptor

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图 2 拦截弹对抗目标示意图

Figure 2. Schematic diagram of interceptor against target

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图 3 预测制导流程^[19-21]

Figure 3. Predictive guidance flowchart^[19-21]

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图 4 标准弹道族

Figure 4. A bunch of standard trajectories

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图 5 拦截示意图

Figure 5. Schematic diagram of interception

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图 6 不同射程拦截对比

Figure 6. Comparison of interception with different ranges

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图 7 远距离拦截示例

Figure 7. An example of long-range interception

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图 8 抛物线近似标准弹道情况

Figure 8. Parabolic approximation of standard trajectory

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图 9 系数a、b、c拟合情况(射程：0~200 km)

Figure 9. Fitting of coefficient a, b and c (Range: 0-200 km)

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图 10 系数a、b、c拟合情况(射程：200~400 km)

Figure 10. Fitting of coefficient a, b and c (Range: 200-400 km)

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图 11 系数a、b、c拟合情况(射程：400~600 km)

Figure 11. Fitting of coefficient a, b and c (Range: 400-600 km)

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图 12 抛物线近似x-t情况

Figure 12. Parabolic approximation of x-t

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图 13 系数a₂、b₂、c₂拟合情况

Figure 13. Fitting of coefficient a₂, b₂ and c₂

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图 14 三维拦截仿真图例(射程：50 km及600 km)

Figure 14. Examples of 3D interception simulation (Range: 50 km and 600 km)

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图 15 纵平面内拦截情况

Figure 15. Interception in vertical plane

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图 16 拦截弹速度

Figure 16. Velocity of interceptor

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图 17 拦截弹高度

Figure 17. Altitude of interceptor

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图 18 拦截弹与目标的弹下点

Figure 18. Projective point of interceptor and target

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图 19 不确定性仿真的脱靶量

Figure 19. Miss distance of uncertainty simulation

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图 20 预测制导程序流程

Figure 20. Flowchart of predictive guidance program

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表 1 助推器参数

Table 1. Parameters of boosters

级数	质量/kg	推力/kN	燃烧时间/s
1	860	80	30
2	170	30	8

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表 2 程序运行时间对比

Table 2. Program run time comparison

仿真次数	设定迭代飞行时间法运行时间/s	设定迭代飞行时间法脱靶量/m	设定预测命中点法运行时间/s	设定预测命中点法脱靶量/m	运行时间节省比例/%	脱靶量减少比例/%
1	28.72	96.89	23.21	16.21	19.19	83.27
2	29.17	293.83	23.29	83.85	20.16	71.46
3	29.22	79.10	23.39	79.10	19.95	0
4	29.14	296.38	22.90	174.68	21.41	41.06
5	29.32	99.86	22.45	79.49	23.43	20.40
6	29.03	178.72	23.26	199.82	19.88	-11.81
7	28.88	251.91	23.12	311.36	19.94	-23.60

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表 3 不同射程拦截仿真结果

Table 3. Simulation results of interception with different ranges

设定的预测命中点			射程/km	脱靶量/m	终点			拦截点偏移/m	末速度/ (m·s^-1)
x坐标/m	y坐标/m	z坐标/m	射程/km	脱靶量/m	x坐标/m	y坐标/m	z坐标/m	拦截点偏移/m	末速度/ (m·s^-1)
-34 862	48 202	-35 956	50.09	15.79	-34 870	48 188	-35 965	19	4 686.31
-69 770	47 692	-71 961	100.02	19.06	-69 626	47 677	-71 812	208	4 066.02
-110 274	46 608	-113 736	158.42	28.24	-110 274	46 636	-113 736	29	3 164.37
-138 417	45 542	-142 763	198.54	36.85	-138 200	45 514	-142 540	312	2 781.90
-173 091	43 878	-178 526	248.31	81.13	-172 846	43 810	-178 273	359	2 587.59
-218 956	41 080	-225 831	314.38	23.63	-218 838	41 112	-225 709	173	2 566.10
-243 346	39 316	-250 987	349.59	63.27	-243 350	39 379	-250 991	63	2 598.21
-277 268	36 542	-285 973	398.33	86.28	-277 275	36 628	-285 981	86	2 660.54
-320 014	32 516	-330 062	460.45	194.60	-320 514	32 270	-330 577	759	2 740.87
-349 067	29 441	-360 027	502.05	199.82	-349 473	29 596	-360 446	604	2 796.76
-386 483	25 077	-398 618	554.99	1.57	-386 325	25 095	-398 455	228	2 838.07
-432 395	19 101	-445 971	620.12	385.45	-431 661	19 588	-445 214	1 161	2 834.60

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表 4 设定的预测命中点坐标

Table 4. Expected predicted impact point coordinate

序号	x/m	y/m	z/m
1	-34 862	48 202	-35 956
2	-69 770	47 692	-71 961
3	-138 417	45 542	-142 763
4	-277 268	36 542	-285 973

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表 5 存在航路捷径时的脱靶量

Table 5. Miss distance with course shortcut

航路捷径/km	脱靶量/m
航路捷径/km	点1	点2	点3	点4
0	3.64	19.06	36.85	86.28
50	6.05	4.85	33.76	118.10
100	36.12	82.94	24.95	134.39
150	178.31	75.37	33.20	258.81
200	87.18	124.92	71.07	449.50
250	55.86	42.33	127.59	415.55
300	37.56	52.74	153.13	326.55
350	95.33	104.96	217.85	135.17
400	180.90	191.41	353.20	128.68
450	260.17	230.11	225.70
500	260.78	168.21	109.11
550	125.82	103.70	167.82
600	319.18	377.57

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表 6 不确定性仿真结果

Table 6. Uncertainty simulation results

射程/km	无噪声脱靶量/m	有噪声平均脱靶量/m	有噪声脱靶量标准差/m	平均飞行时间/s	有噪声脱靶量最大值/m
158.42	28.24	27.94	2.08	69.73	32.66
349.59	63.27	83.21	11.25	147.65	118.10
554.99	1.57	18.04	13.02	210.51	60.86
620.12	385.45	384.89	23.31	228.39	435.42

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