Journal of Systems Engineering and Electronics ›› 2023, Vol. 34 ›› Issue (4): 1020-1032.doi: 10.23919/JSEE.2023.000091
• • 上一篇
-
收稿日期:2021-11-24出版日期:2023-08-18发布日期:2023-08-28
Optimal maneuver strategy to improve the observability of angles-only rendezvous
Ronghua DU(
), Wenhe LIAO(), Xiang ZHANG()
- 1 School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China
-
Received:2021-11-24Online:2023-08-18Published:2023-08-28 -
Contact:Wenhe LIAO E-mail:Duronghua1995@126.com;cnwho@mail.njust.edu.cn;zhxiang2002@126.com -
About author:
DU Ronghua was born in 1995. He received his B.S. degree in mechanical engineering from the School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing, China, in 2017. He is pursuing his Ph.D. degree in mechanical engineering from the School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing, China. Since 2017, he has studied in the the Micro Satellite Research Centre and has been a postgraduate with the School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing, China. His research interests include satellite attitude determination, vision-based relative navigation, guidance navigation and control, and angles-only relative navigation. E-mail: Duronghua1995@126.com
LIAO Wenhe was born in 1965. He received his B.S. degree in aerospace manufacturing engineering from the School of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China, in 1990 and Ph.D. degree in aerospace manufacturing engineering from the School of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China, in 1996. He is currently the Vice President of the Nanjing University of Science and Technology, Nanjing, China. He is also the Director of the Micro Satellite Research Centre and a professor with the School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing, China. His research interests include satellite system design and high-end equipment design. E-mail: cnwho@mail.njust.edu.cn
ZHANG Xiang was born in 1973. He received his B.S. degree in aerospace manufacturing engineering from the School of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China, in 1998 and Ph.D. degree in aerospace manufacturing engineering from the School of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China, in 2007. He is currently the Deputy Director of the Micro Satellite Research Centre and a professor with the School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing, China. His research interests include satellite system design, satellite attitude control, satellite payloads, and ground stations. E-mail: zhxiang2002@126.com -
Supported by:This work was supported by the China Aerospace Science and Technology Corporation 8th Research Institute Industry-University-Research Cooperation Fund (SAST 2020-019)
引用本文
. [J]. Journal of Systems Engineering and Electronics, 2023, 34(4): 1020-1032.
Ronghua DU, Wenhe LIAO, Xiang ZHANG. Optimal maneuver strategy to improve the observability of angles-only rendezvous[J]. Journal of Systems Engineering and Electronics, 2023, 34(4): 1020-1032.
"
"
"
"
"
"
"
| Parameter | Value |
| Absolute orbital elements of the space target (a/km, e, i/(°), Ω/(°), ω/(°), M/(°)) | (6878.137, 0, 40, 120, 0, 50) |
| ROE1 (aδa, aδλ, aδex, aδey, aδix, aδiy)/km | (0, −30, 0.5, 0, −0.5, 0) |
| ROE2 (aδa, aδλ, aδex, aδey, aδix, aδiy)/km | (−0.15, −20, 0.3, 0, −0.3, 0) |
| ROE3 (aδa, aδλ, aδex, aδey, aδix, aδiy)/km | (0, −5, 0, 0, 0, 0) |
| Sample period T/s | 10 |
| Simulation time | 1000 |
| Sensor measurement noise (σα = σε)/arcsec | 30 |
"
"
"
"
"
"
"
| 1 |
SEARS P J, HO J Impact evaluation of in-space additive manufacturing and recycling technologies for on-orbit servicing. Journal of Spacecraft and Rockets, 2018, 55 (4): 1498- 1508.
doi: 10.2514/1.A34135 |
| 2 |
CHIU S W Promoting international cooperation in the age of global space governance: a study on on-orbit servicing operations. Acta Astronautica, 2019, 161, 375- 381.
doi: 10.1016/j.actaastro.2018.07.019 |
| 3 |
RAZZAGHI P, KHATIB E A, BAKHTIARI S Sliding mode and SDRE control laws on a tethered satellite system to de-orbit space debris. Advances in Space Research, 2019, 64 (1): 18- 27.
doi: 10.1016/j.asr.2019.03.024 |
| 4 |
CHU Z Y, WEI T, SHEN T, et al Optimal commands based multi-stage drag de-orbit design for a tethered system during large space debris removal. Acta Astronautica, 2019, 163, 238- 249.
doi: 10.1016/j.actaastro.2018.12.038 |
| 5 |
ZHU Z H, GUO Y Adaptive coordinated attitude control for spacecraft formation with saturating actuators and unknown inertia. Journal of the Franklin Institute, 2019, 356, 1021- 1037.
doi: 10.1016/j.jfranklin.2018.02.021 |
| 6 |
IVANOV D, KUSHNIRUK M, OVCHINNIKOV M Study of satellite formation flying control using differential lift and drag. Acta Astronautica, 2018, 152, 88- 100.
doi: 10.1016/j.actaastro.2018.07.047 |
| 7 |
MITCHELL A, PIMENTA D, GILL J, et al Cardiovascular effects of space radiation: implications for future human deep space exploration. European Journal of Preventive Cardiology, 2019, 26 (16): 1707- 1714.
doi: 10.1177/2047487319831497 |
| 8 |
LI H, ZHANG Q Y, ZHANG N T Autonomous navigation of formation flying spacecrafts in deep space exploration and communication by hybrid navigation utilizing neural network filter. Acta Astronautica, 2009, 65, 1028- 1031.
doi: 10.1016/j.actaastro.2009.03.038 |
| 9 | HAN J, LI W X, FENG K, et al Vision-based aerial image mosaicking algorithm with object detection. Journal of Systems Engineering and Electronics, 2022, 33 (2): 259- 268. |
| 10 |
GONG B C, LI W D, LI S, et al Angles-only initial relative orbit determination algorithm for non-cooperative spacecraft proximity operations. Astrodynamics, 2018, 2, 217- 231.
doi: 10.1007/s42064-018-0022-0 |
| 11 | GAIAS G, ARDAENS J S Flight demonstration of autonomous non-cooperative rendezvous in low earth orbit. Journal of Guidance, Control and Dynamics, 2018, 41, 1137- 1154. |
| 12 | D’AMICO S, PAVONE M, SARAF S, et al. Miniaturized autonomous distributed space systems for future science and exploration. Proc. of the 8th International Workshop of Spacecraft Formation Flying, 2015. https://elib.dlr.de/98200/. |
| 13 |
GELLER D K, PEREZ A C Initial relative orbit determination for close-in proximity operations. Journal of Guidance, Control and Dynamics, 2015, 38, 1833- 1841.
doi: 10.2514/1.G000933 |
| 14 |
GRZYMISCH J, FICHTER W Observability criteria and unobservable maneuvers for in-orbit bearings-only navigation. Journal of Guidance, Control and Dynamics, 2014, 37 (4): 1250- 1259.
doi: 10.2514/1.62476 |
| 15 |
GRZYMISCH J, FICHTER W Optimal rendezvous guidance with enhanced bearings-only observability. Journal of Guidance, Control and Dynamics, 2015, 38 (6): 1131- 1139.
doi: 10.2514/1.G000822 |
| 16 |
GELLER D K, KLEIN I Angles-only navigation state observability during orbital proximity operations. Journal of Guidance, Control and Dynamics, 2014, 37 (6): 1976- 1983.
doi: 10.2514/1.G000133 |
| 17 | NEWMAN B, LOVELL T A, PRATT E, et al. Quadratic hexa-dimensional solution for relative orbit determination. Proc. of the AIAA/AAS Astrodynamics Specialist Conference, 2014. https://www.webofscience.com/wos/alldb/full-record/wos:00371647200201. |
| 18 |
PEREZ A C, GELLER D K, LOVELL T A Non-iterative angles-only initial relative orbit determination with J2 perturbations . Acta Astronautica, 2018, 151, 146- 159.
doi: 10.1016/j.actaastro.2018.06.033 |
| 19 | WOFFINDEN D C, GELLER D K Observability criteria for angles-only navigation. IEEE Trans. on Aerospace and Electronic System, 2009, 45 (3): 1194- 1208. |
| 20 |
ARDAENS J S, GAIAS G A numerical approach to the problem of angles-only initial relative orbit determination in low earth orbit. Advances in Space Research, 2019, 63 (12): 3884- 3899.
doi: 10.1016/j.asr.2019.03.001 |
| 21 |
ROSCOE C, WESTPHAL J, GRIESBACH J, et al Formation establishment and reconfiguration using differential elements in J2-perturbed orbits . Journal of Guidance, Control and Dynamics, 2015, 38 (9): 1725- 1740.
doi: 10.2514/1.G000999 |
| 22 |
GAIAS G, D’AMICO S, ARDAENS J S Generalized multi-impulsive maneuvers for optimum spacecraft rendezvous in near-circular orbit. International Journal of Space Science and Engineering, 2015, 3 (1): 68- 88.
doi: 10.1504/IJSPACESE.2015.069361 |
| 23 |
CHERNICK M, D’AMICO S New closed-form solutions for optimal impulsive control of spacecraft relative motion. Journal of Guidance, Control, and Dynamics, 2018, 41 (2): 301- 319.
doi: 10.2514/1.G002848 |
| 24 | KOENIG A, GUFFANTI T, D’AMICO S. New state transition matrices for relative motion of spacecraft formations in perturbed orbits. Proc. of the AIAA/AAS Astrodynamics Specialist Conference, 2016: 1749−1768. |
| 25 |
GAIAS G, ARDAENS J S, MONTENBRUCK O Model of J2 perturbed satellite relative motion with time-varying differential drag . Celestial Mechanics and Dynamical Astronomy, 2015, 123 (4): 411- 433.
doi: 10.1007/s10569-015-9643-2 |
| 26 |
VADDI S, ALFRIEND K, VADALI S, et al Formation establishment and reconfiguration using impulsive control. Journal of Guidance, Control and Dynamics, 2005, 28 (2): 262- 268.
doi: 10.2514/1.6687 |
| 27 |
GRZYMISCH J, FICHTER W Analytic optimal observability maneuvers for in-orbit bearings-only rendezvous. Journal of Guidance, Control and Dynamics, 2014, 37 (5): 1658- 1664.
doi: 10.2514/1.G000612 |
| 28 |
DAVIS C Theory of positive linear dependence. American Journal of Mathematics, 1954, 76 (4): 733- 746.
doi: 10.2307/2372648 |
| 29 | BOYD S, VANDENBERGHE L. Convex optimization. Cambridgeshire: Cambridge University Press, 2004. |
| 30 |
YIN J F, HAN C Elliptical formation control based on relative orbit elements. Chinese Journal of Aeronautics, 2013, 26, 1554- 1567.
doi: 10.1016/j.cja.2013.07.014 |
| 31 |
GAIAS G, D’AMICO S, ARDAENS J S Angles-only navigation to a non-cooperative satellite using relative orbital elements. Journal of Guidance, Control and Dynamics, 2014, 37 (2): 439- 451.
doi: 10.2514/1.61494 |
| 32 | BATTIN R H. An introduction to the mathematics and methods of astrodynamics. Reston: American Institute of Aeronautics & Astronsutics, 1999. |
| No related articles found! |
| 阅读次数 | ||||||
|
全文 |
|
|||||
|
摘要 |
|
|||||