Investigation and analysis of phase change orbital maneuver in different anomalies in orbital rendezvous mission
Document Type : Original Article
Authors
1
Malek Ashtar University of Technology, Aerospace Department
2
Malek Ashtar University of Technology
Abstract
Phase orbital maneuvers with the goal of rendezvous are a series of orbital adjustments made by a spacecraft to align its orbit with another object, such as another spacecraft or space station. These maneuvers usually involve adjusting the speed and trajectory of the spacecraft to gradually decrease the distance and match the target orbit at a certain time. If the orbital phase adjustment is without regard to specific time (non-orbital rendezvous), the problem is greatly simplified, but in the case of specific time (phase change in a specific period of time), the problem becomes complicated and can be analyzed by two objectives including, fuel consumption and elapsed time. In this research, the influence of the location of performing the phase change maneuver in a circular orbit has been investigated by various true anomalies. Based on the results, from 0 to 10 degree true anomaly, the duration of the maneuver increases with a very large slope, and after that, the duration of the maneuver decreases until the anomaly of 270 degrees.
Keywords
Subjects
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[12] کیانی م, شکوری ا, پورتاکدوست سح, سینجلی م. بهینهسازی انتقال مداری چندضربه ای با استفاده از روش شبه نیوتن. علوم و فناوری فضایی. 2018 May 22;11(1):49-57.
[13] موسوی م، جعفری م، دلالت م "طراحی الگوریتم اصلاح مداری یک منظومه ماهوارهای منطقهای مدار پایین زمین" پایان نامه کارشناسی ارشد ،دانشگاه صنعتی مالک اشتر, تهران,زمستان 1402.
[2] A. M. Kaki S, "Spacecraft rendezvous in closed keplerian orbits using constant radial thrust acceleration.," Journal of Guidance, Control, and Dynamics., 2023 Jun;46(6):1112-25..
[3] M. Tyler-Rodrigue, " Spacecraft Orbital Rendezvous using Convex Optimization. Diss.," ResearchSpace@ Auckland, , 2023..
[4] L. C. Davide Costigliola, "Autonomous Phasing Maneuvers in Near Circular Earth Orbits," Conference: 2022 AAS/AIAA Astrodynamics Specialist Conference, Carolina, USA, August 2022.
[5] P. N. V. Giuseppe Narducci, "Analysis of phasing maneuver performed by a solar electric platform," Politecnico di, Torino, April 2020.
[6] W. S. W. W. Shang H, "Design and optimization of low-thrust orbital phasing maneuver.," Aerospace Science and Technology., 2015.
[7] Y.-z. L. ,. J. Z. ,. H.-y. L. ,. G.-j. T. Li-bo Liang1, "Rendezvous-Phasing Errors Propagation Using Quasi-linearization Method," AIAA Guidance, Navigation, and Control Conference, Changsha, China,, August 2010,.
[8] T. G.-J. L. Y.-J. L. H.-Y. Luo Y-Z, "Optimization of multiple-impulse, multiple-revolution, rendezvous-phasing maneuvers.," Journal of Guidance, Control, and Dynamics. , 2007.
[9] G.-J. T. Ya-Zhong Luo, "Rendezvous phasing special-point maneuvers mixed discrete-continuous optimization using simulated annealing," Aerospace Science and Technology,, vol. Volume 10, no. Issue 7, pp. Pages 652-658, 2006.
[10] C.-P. V. Hall CD, "Minimum-time orbital phasing maneuvers.," Journal of guidance, control, and dynamics., 2003.
[11] طائی ح, حجت, شکرالهی, پوریا. بکارگیری رویکردهای بهینهسازی چندهدفه در طراحی کنترلکننده بهینه برای عملیات الحاق مداری با درنظر گرفتن دینامیک عملگرها و مقایسه نتایج. علوم و فناوری فضایی. 2020 Jun 21;13(2):87-96.
[12] کیانی م, شکوری ا, پورتاکدوست سح, سینجلی م. بهینهسازی انتقال مداری چندضربه ای با استفاده از روش شبه نیوتن. علوم و فناوری فضایی. 2018 May 22;11(1):49-57.
[13] موسوی م، جعفری م، دلالت م "طراحی الگوریتم اصلاح مداری یک منظومه ماهوارهای منطقهای مدار پایین زمین" پایان نامه کارشناسی ارشد ،دانشگاه صنعتی مالک اشتر, تهران,زمستان 1402.
Volume 4, Issue 2
March 2025Pages 81-90
- Receive Date 10 July 2024
- Revise Date 13 September 2024
- Accept Date 04 January 2025