Journal of Systems Engineering and Electronics ›› 2018, Vol. 29 ›› Issue (6): 1284-1292.doi: 10.21629/JSEE.2018.06.15
• Control Theory and Application • Previous Articles Next Articles
Kai ZHANG1(), Jiajun XIONG2,*(), Tingting FU2()
Received:
2017-09-27
Online:
2018-12-25
Published:
2018-12-26
Contact:
Jiajun XIONG
E-mail:christophzhang@163.com;jiajunxiong@yahoo.com;124611796@qq.com
About author:
ZHANG Kai was born in 1990. He received his B.S. degree from School of Aerospace Science and Engineering, National University of Defense Technology in 2014. He is currently working toward his Ph.D. degree in the Air Force Early Warning Academy. So far he has published more than ten papers, in which three papers are indexed by EI. His research interests include information fusion and hypersonic vehicle tracking. E-mail: Supported by:
Kai ZHANG, Jiajun XIONG, Tingting FU. Coupled dynamic model of state estimation for hypersonic glide vehicle[J]. Journal of Systems Engineering and Electronics, 2018, 29(6): 1284-1292.
Table 3
Performance comparison of state estimation errors"
Type | Example | Case 1 | Case 2 | Case 3 | Case 4 |
Position/m | MM | 107.8 | 102.7 | 192.0 | 167.6 |
SM | 105.7 | 101.5 | 187.4 | 160.3 | |
BM | 97.00 | 92.54 | 171.3 | 142.6 | |
GM | 78.11 | 74.05 | 151.3 | 132.6 | |
Velocity/(m/s) | MM | 23.94 | 22.85 | 37.12 | 33.59 |
SM | 23.00 | 21.47 | 32.65 | 32.89 | |
BM | 19.34 | 18.71 | 26.80 | 26.48 | |
GM | 18.64 | 17.34 | 26.83 | 23.48 | |
MM | 7.069 | 6.904 | 9.132 | 18.04 | |
SM | 6.770 | 6.548 | 8.585 | 17.49 | |
BM | 1.861 | 1.811 | 2.047 | 12.56 | |
GM | 2.861 | 2.659 | 4.097 | 15.82 | |
MM | 80.85 | 76.20 | 86.51 | 100.7 | |
SM | 77.95 | 75.25 | 83.78 | 97.70 | |
BM | 71.22 | 69.94 | 76.37 | 89.97 | |
GM | 67.76 | 65.13 | 70.38 | 85.87 | |
MM | 19.86 | 17.07 | 21.82 | 23.25 | |
SM | 20.06 | 19.05 | 22.18 | 23.32 | |
BM | 17.50 | 17.80 | 18.35 | 19.41 | |
GM | 14.20 | 15.56 | 16.97 | 17.50 |
1 | PAUL L M, VINCENT L R, LUAT T N, et al. NASA hypersonic fight demonstration overview, status, and future plans. Acta Astronautica, 2004, 55 (7): 619- 630. |
2 | DARPA. Tactical boost glide broad agency announcement. DARPA-BAA-14-24, 2014. |
3 |
MAHAPATRA P R, MEHROTRA K. Mixed coordinate tracking of generalized maneuvering targets using acceleration and jerk models. IEEE Trans. on Aerospace and Electronic Systems, 2000, 36 (3): 992- 1000.
doi: 10.1109/7.869519 |
4 | LI X R, JILKOV V P. Survey of maneuvering target tracking. IEEE Trans. on Aerospace and Electronic Systems, 2004, 39 (4): 1333- 1364. |
5 |
GHOSH S, BHATTACHARYYA A K, MUKHOPADHYAY S, et al. Improved estimation of kinematic state of reentry ballistic targets with modeling of colored and nonstationary seeker noise. IEEE Trans. on Aerospace and Electronic Systems, 2012, 48 (4): 3186- 3206.
doi: 10.1109/TAES.2012.6324691 |
6 | SUN T, XIN M. Hypersonic entry vehicle state estimation using nonlinearity-based adaptive cubature Kalman filters. Acta Astronautica, 2017, 134 (3): 221- 230. |
7 | WANG G H, LI J J, ZHANG X Y, et al. A tracking model of near space hypersonic slippage leap maneuvering target. Acta Aeronautica et Astronautica Sinica, 2015, 36 (7): 2400- 2410. |
8 | ZHANG X Y, WANG G H, LI J, et al. Tracking of hypersonic sliding target in near-space. Acta Aeronautica et Astronautica Sinica, 2015, 36 (6): 1983- 1994. |
9 | ZHANG X Y, WANG G H, JING Z, et al. Tracking of hypersonic boost-to-glide trajectory target in near-space. Journal of Astronautics, 2015, 36 (10): 1125- 1132. |
10 | NIE X H, ZHANG F M, XU Y M. Adaptive model algorithm for maneuvering target tracking of NSHV. Systems Engineering and Electronics, 2016, 38 (3): 506- 511. |
11 |
LIANG Y Q, HAN C Z. Hybrid state estimation and modelset design of invariable-structure semi-ballistic reentry vehicle. Science China: Information Sciences, 2011, 54 (4): 812- 823.
doi: 10.1007/s11432-010-4159-6 |
12 | LIANG Y Q, HAN C Z, SUN Y J, et al. Modeling and multiple-model estimation of invariable-structure semiballistic reentry vehicle. Acta Automatica Sinica, 2011, 37 (6): 700- 712. |
13 | QIN L, LI J L, ZHOU D. Tracking filter algorithm for near space target based on AGIMM. Systems Engineering and Electronics, 2015, 37 (5): 1009- 1014. |
14 | QIN L, LI J L, ZHOU D. Tracking for near space target based on IMM algorithm. Systems Engineering and Electronics, 2014, 36 (7): 1243- 1249. |
15 |
LI X R, JILKOV V P. Survey of maneuvering target tracking. IEEE Trans. on Aerospace and Electronic Systems, 2010, 46 (1): 96- 119.
doi: 10.1109/TAES.2010.5417150 |
16 | MINVIELLE P. Decades of improvements in re-entry ballistic vehicle tracking. IEEE Aerospace & Electronic Systems Magazine, 2005, 20 (8): CF/1- CF14. |
17 |
FARINA A, RISTIC B, BENVENUTI D. Tracking a ballistic target: comparison of several nonlinear filters. IEEE Trans. on Aerospace and Electronic Systems, 2002, 38 (3): 854- 867.
doi: 10.1109/TAES.2002.1039404 |
18 | OLIVIER D M, ROBERT H B. Tracking and identification of a maneuvering reentry vehicle. Proc. of the AIAA Guidance, Navigation, and Control Conference and Exhibit, 2003: 1-11. |
19 | ZHANG S C, HU G D. Target tracking for maneuvering reentry vehicles with interactive multiple model unscented Kalman filter. Acta Automatica Sinica, 2007, 33 (11): 1120- 1125. |
20 |
KIM J, VADDI S S, MENON P K, et al. Comparison between nonlinear filtering techniques for spiraling ballistic missile state estimation. IEEE Trans. on Aerospace and Electronic Systems, 2012, 48 (1): 313- 328.
doi: 10.1109/TAES.2012.6129638 |
21 | KIM J, MENON P, OHLMEYER E. Motion models for use with the maneuvering ballistic missile tracking estimators. Proc. of the AIAA Guidance, Navigation, and Control Conference, 2010: AIAA 2010-7589. |
22 | ZHANG K, XIONG J J, HAN C Y, et al. A tracking algorithm of hypersonic glide reentry vehicle via aerodynamic model. Journal of Astronautics, 2017, 38 (2): 123- 130. |
23 | WU N, CHEN L. Adaptive Kalman filtering for trajectory estimation of hypersonic glide reentry vehicles. Acta Aeronautica et Astronautica Sinica, 2013, 34 (8): 1960- 1971. |
24 | MOON K R, KIM T H, SONG T L. Comparison of ballisticcoefficient-based estimation algorithms for precise tracking of a re-entry vehicle and its impact point prediction. Journal of Astronomy & Space Sciences, 2012, 29 (4): 363- 374. |
25 |
GHOSH S, MUKHOPADHYAY S. Tracking reentry ballistic targets using acceleration and jerk models. IEEE Trans. on Aerospace and Electronic Systems, 2011, 47 (1): 666- 683.
doi: 10.1109/TAES.2011.5705698 |
26 | ZHOU Z, LIU J M, GUO X K. Adaptive tracking algorithm for reentry vehicle based on stochastic model approximation. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40 (5): 651- 657. |
27 | HOUGH M E. Reentry maneuver estimation using nonlinear Markov acceleration models. Journal of Guidance, Control and Dynamics, 2017, 40 (7): 1- 18. |
28 | KARELAHTI J, VIRTANEN K. Adaptive controller for the avoidance of an unknownly guided air combat missile. Proc. of the 46th IEEE Conference on Decision and Control, 2008: 1306-1313. |
29 | ZOU X G, ZHOU D, DU R L, et al. PN guidance law identification using multi-model adaptive estimation. Journal of Astronautics, 2016, 37 (8): 619- 630. |
30 | WEISS S S. Identification of nonlinear aerodynamic derivatives using classical and extended local model networks. Aerospace Science and Technology, 2010, 42 (1): 1- 12. |
31 | REGAN F J, ANANDAKRISHNAN S M. Dynamics of atmospheric re-entry. New York: AIAA, 1993. |
32 | PHILLIPS T H. A common aero vehicle (CAV) model, description, employment guide. Arlington: Schafer Corporation for AFRL and AF-SPC, 2003. |
[1] | Keyi LI, Zhengkun GUO, Gongjian ZHOU. State estimation in range coordinate using range-only measurements [J]. Journal of Systems Engineering and Electronics, 2022, 33(3): 497-510. |
[2] | Muhammad WASIM, Ahsan ALI. Airship aerodynamic model estimation using unscented Kalman filter [J]. Journal of Systems Engineering and Electronics, 2020, 31(6): 1318-1329. |
[3] | Haoran SHI, Faxing LU, Hangyu WANG, Junfei XU. Optimal observation configuration of UAVs based on angle and range measurements and cooperative target tracking in three-dimensional space [J]. Journal of Systems Engineering and Electronics, 2020, 31(5): 996-1008. |
[4] | Junyi Zuo and Xiaoping Zhong. Particle filter for nonlinear systems with multi-sensor asynchronous random delays [J]. Journal of Systems Engineering and Electronics, 2017, 28(6): 1064-1071. |
[5] | Wei Wang, Dan Li, and Liping Jiang. Best linear unbiased estimation algorithm with Doppler measurements in spherical coordinates [J]. Systems Engineering and Electronics, 2016, 27(1): 128-. |
[6] | Binglong Chen and Yunhai Geng. Modified super twisting controller for servicing to uncontrolled spacecraft [J]. Journal of Systems Engineering and Electronics, 2015, 26(2): 334-345. |
[7] | Fang Deng, Jie Chen, and Chen Chen. Adaptive unscented Kalman filter for parameter and state estimation of nonlinear high-speed objects [J]. Journal of Systems Engineering and Electronics, 2013, 24(4): 655-665. |
[8] | Yuanwen Zhang, Leping Yang, Yanwei Zhu, and Huan Huang. Dynamics and nonlinear control of space electromagnetic docking [J]. Journal of Systems Engineering and Electronics, 2013, 24(3): 454-. |
[9] | Mei Liu, Jianguo Yu, Ling Yang, Lu Yao, and Yaosheng Zhang. Consecutive tracking for ballistic missile based on bearings-only during boost phase [J]. Journal of Systems Engineering and Electronics, 2012, 23(5): 700-707. |
[10] | Guo Lei, Tang Bin & Liu Gang. Posterior Cramer-Rao lower bounds for bearing-only tracking [J]. Journal of Systems Engineering and Electronics, 2008, 19(1): 27-32. |
[11] | Zhan Ronghui, Wang Ling, Wan Jianwei & Sun Zhongkang. Passive target tracking using marginalized particle filter [J]. Journal of Systems Engineering and Electronics, 2007, 18(3): 503-508. |
Viewed | ||||||
Full text |
|
|||||
Abstract |
|
|||||