基于高程异常补偿的飞机终端区组合导航高度优化算法

doi:10.12305/j.issn.1001-506X.2021.09.30

Abstract

Abstract:

The instrument landing system (ILS) is used for aircraft approaching and landing in the terminal area of most large airports. However, due to price and usage environment, some airports are not equipped with ILS. Aiming at the airport terminal area not equipped with ILS, a method of using the error judgment factor is proposed. Combined with the height anomaly compensation algorithm, the combination of the air data system (ADS), strapdown inertial navigation system (SINS) and Beidou navigation system (BDS) are used to optimize the altitude calculation algorithm for improving the height accuracy during aircraft approaching. A new Kalman filter altitude measurement equation is established by combining the elevation anomalies in the airport terminal area to optimize and simulate the altitude positioning algorithm of the integrated navigation system. The simulation results show that the algorithm not only reduces the BDS height error significantly through the height anomaly compensation in the terminal area, but also suppresses the divergence of the SINS error. The error of height positioning after combination affected by the static pressure source error can reduce 41.52% compared with the single system. The algorithm improves the high positioning accuracy.

Key words: height anomaly, integrated navigation, Kalman filter, approaching and landing, static pressure source error

CLC Number:

TP202.7

Shuguang SUN, Qixin WEN. Aircraft height optimization algorithm of integrated navigation in terminal area based on height anomaly compensation[J]. Systems Engineering and Electronics, 2021, 43(9): 2612-2619.

Figures/Tables 10

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References 29

1	QU C Q . Research on signal of field monitor of 7220A localizer beacon subsystem of ILS[J]. Open Journal of Antennas & Propagation, 2015, 3 (4): 37- 50.
2	汪媛卿. 低空环境下民用航空器精密进近算法研究[D]. 上海: 上海交通大学, 2012.
	WANG Y Q. Civil aircraft precision approach and algorithm research in low altitude environment[D]. Shanghai: Shanghai Jiao Tong University, 2012.
3	刘健, 曹冲. 全球卫星导航系统发展现状与趋势[J]. 导航定位学报, 2020, 8 (1): 5- 12.
	LIU J , CAO C . Development status and trend of global navigation satellite system[J]. Journal of Navigation and Positioning, 2020, 8 (1): 5- 12.
4	ZRINJSKI M , BARKOVI U , MATIKA K . Development and mo-dernization of GNSS[J]. Geodetski List, 2019, 73 (96): 45- 65.
5	HE K F , WENG D J , JI S Y , et al. Improving the performance of time-relative GNSS precise positioning in remote areas[J]. Sensors, 2021, 21 (1): 292- 293. doi: 10.3390/s21010292
6	冯翔, 张斌. 数字化仪表着陆系统发射通道校准算法[J]. 计算机应用, 2017, 37 (3): 741- 745.
	FENG X , ZHANG B . Transmission channel calibration algorithm for digital instrument landing system[J]. Journal of Computer Applications, 2017, 37 (3): 741- 745.
7	FELUX M, DAUTERMANN T, BECKER H. GBAS approach guidance performance-A comparison to ILS[C]//Proc. of the International Technical Meeting of the Institute of Navigation, 2013: 4-9.
8	LI R , ZHENG S Y , WANG E S , et al. Advances in BeiDou navigation satellite system (BDS) and satellite navigation augmentation technologies[J]. Satellite Navigation, 2020, 1 (11): 3- 12.
9	LU Z P , WEI Z Q , LI J , et al. Grid model for high-accuracy coordinate transformation of china geodetic coordinate system 2000[J]. Acta Geodaetica et Cartographica Sinica, 2019, 2 (1): 17- 25.
10	ALI B S , TAIB N A . A study on geometric and barometric altitude data in automatic dependent surveillance broadcast (ADS-B) messages[J]. The Journal of Navigation, 2019, 72 (5): 1140- 1158. doi: 10.1017/S0373463319000201
11	PEREZ R O . Ionospheric error contribution to GNSS single-frequency navigation at the 2014 solar maximum[J]. Journal of Geodesy, 2017, 91 (4): 397- 407. doi: 10.1007/s00190-016-0971-0
12	SHE C L , YUE X N , HU L H , et al. Estimation of ionospheric total electron content from a multi-GNSS station in China[J]. IEEE Trans.on Geoscience and Remote Sensing, 2019, 58 (2): 852- 860.
13	WANG M , CHAI H Z , LIU J , et al. BDS relative static positioning over long baseline improved by GEO multipath mitigation[J]. Advances in Space Research, 2016, 57 (3): 782- 793. doi: 10.1016/j.asr.2015.11.032
14	LI X , GUO J M , ZHOU L . Performance analysis of BDS/GPS kinematic vehicle positioning in various observation conditions[J]. Sensor Review, 2016, 36 (3): 249- 256. doi: 10.1108/SR-12-2015-0198
15	NING X L , YUAN W P , LIU Y H . A tightly coupled rotational SINS/CNS integrated navigation method for aircraft[J]. Journal of Systems Engineering and Electronics, 2019, 30 (4): 770- 782. doi: 10.21629/JSEE.2019.04.14
16	LOU T S , CHEN N H , CHEN Z W , et al. Robust partially strong tracking extended consider Kalman filtering for INS/GNSS integrated navigation[J]. IEEE Access, 2019, 7, 151230- 151238. doi: 10.1109/ACCESS.2019.2948229
17	LIU D , WANG H J , XIA Q Y , et al. A low-cost method of improving the GNSS/SINS integrated navigation system using multiple receivers[J]. Electronics, 2020, 9 (7): 3- 22.
18	WANG D J , DONG Y , LI Z Y , et al. Constrained mems-based GNSS/INS tightly coupled system with robust Kalman filter for accurate land vehicular navigation[J]. IEEE Trans.on Instrumentation and Measurement, 2020, 69 (7): 5138- 5148. doi: 10.1109/TIM.2019.2955798
19	GUO M Z , GUO C , ZHANG C . SINS/GNSS-integrated navigation of surface vessels based on various nonlinear Kalman filters and large ship dynamics[J]. Journal of Electrical Engineering and Technology, 2020, 16 (1): 531- 546. doi: 10.1007/s42835-020-00537-z
20	WANG M S, WU W Q, HE X F, et al. State transformation extended Kalman filter for SINS based integrated navigation system[C]//Proc. of the DGON Inertial Sensors and Systems Symposium, 2019.
21	ZHANG C , GUO C , ZHANG D H . Ship navigation via GPS/IMU/LOG integration using adaptive fission particle filter[J]. Ocean Engineering, 2018, 156, 435- 445. doi: 10.1016/j.oceaneng.2018.03.012
22	MA Y , CHEN Y , ZHOU X W , et al. Remain useful life prediction of lithiumion battery based on Gauss-Hermite particle filter[J]. IEEE Trans.on Control Systems Technology, 2018, 27 (4): 1788- 1795.
23	GUO Y H , ZHAN X Q , ZHANG X , et al. GNSS and map-match-ing navigation integrity monitoring for land vehicles[J]. Journal of Aeronautics, Astronautics and Aviation, 2019, 51 (1): 111- 129.
24	程超. 大气数据系统建模及在组合导航中的应用研究[D]. 成都: 电子科技大学, 2019.
	CHENG C. Modeling of air data system and it's application in integrated navigation[D]. Chengdu: University of Electronic Science and Technology of China, 2019.
25	JURADO J D , MCGEHEE C C . Complete online algorithm for air data system calibration[J]. Journal of Aircraft, 2019, 56 (2): 517- 528. doi: 10.2514/1.C034964
26	WANG J M , XIE D P . GPS elevation fitting study based on ternary polynomial regression[J]. Earth Sciences Research Journal, 2020, 24 (2): 201- 205. doi: 10.15446/esrj.v24n2.87228
27	王雪林, 李楠. GPS高程拟合方法研究[J]. 测绘与空间地理信息, 2020, 43 (5): 56- 60, 64.
	WANG X L , LI N . Research on GPS elevation fitting method[J]. Geomatics & Spatial Information Technology, 2020, 43 (5): 56- 60, 64.
28	匡杉. BDS/IN组合导航系统完好性监视性能测试评估平台仿真[D]. 天津: 中国民航大学, 2017.
	KUANG S. The test platform simulation for BDS/INS integrated navigation system integrity monitoring performance eva-luation[D]. Tianjin: Civil Aviation University of China, 2017.
29	何培. 机载大气数据系统静压源误差分析及修正方法的研究[D]. 天津: 中国民航大学, 2014.
	HE P. Analysis and study of correction method for static source error of airborne air data system[D]. Tianjin: Civil Aviation University of China, 2014.

仿真条件设置	具体参数
仿真时间/s	120
滤波周期/s	1
陀螺仪常值漂移/(°/h)	0.2
陀螺仪随机噪声/(°/h)	N(0, 0.02)
加速度计常值漂移/g	1×10^-3
加速度计常值漂移/g	N(0, 1×10^-5)
BDS测量伪距误差/m	N(10, 5)
ADS测量气压误差/Pa	N(0, 50)

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Aircraft height optimization algorithm of integrated navigation in terminal area based on height anomaly compensation

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