Low-Thrust Trajectory Design Using Finite Fourier Series Approximation of Pseudoequinoctial Elements
المؤلفون المشاركون
Wang, Hua
Zhou, Wanmeng
Li, Haiyang
Ding, Ran
المصدر
International Journal of Aerospace Engineering
العدد
المجلد 2019، العدد 2019 (31 ديسمبر/كانون الأول 2019)، ص ص. 1-18، 18ص.
الناشر
Hindawi Publishing Corporation
تاريخ النشر
2019-11-04
دولة النشر
مصر
عدد الصفحات
18
الملخص EN
A new low-thrust trajectory design method is proposed that is based on the finite Fourier series method with pseudoequinoctial elements rather than the more common cylindrical coordinate components.
The bijection relation between the elements and control variables is ensured by introducing an additional equality constraint derived from the angular momentum conservation.
The guidance law and on-line control variables are obtained by applying inverse dynamics and the framework of inverse simulation technology, respectively.
The pseudoequinoctial finite Fourier series method has the advantages of both the Fourier series and the perturbation analysis methods.
For two-body problems, three cases were studied: the Earth to Mars, 1989ML, and Tempel-1 missions.
Regarding the design of a rendezvous trajectory with a large inclination angle and a high eccentricity rate, this method yields a broader range of feasible results than the traditional Fourier series method.
The circular restricted three-body problem was solved for the first time using the pseudoequinoctial finite Fourier series method combined with the patched conics method.
The low-thrust Earth-Moon transfer was analyzed, and the results show that this method improves window analysis efficiency and guarantees precision of the initial geocentric trajectory for the low-thrust transfer.
نمط استشهاد جمعية علماء النفس الأمريكية (APA)
Zhou, Wanmeng& Li, Haiyang& Wang, Hua& Ding, Ran. 2019. Low-Thrust Trajectory Design Using Finite Fourier Series Approximation of Pseudoequinoctial Elements. International Journal of Aerospace Engineering،Vol. 2019, no. 2019, pp.1-18.
https://search.emarefa.net/detail/BIM-1156118
نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)
Zhou, Wanmeng…[et al.]. Low-Thrust Trajectory Design Using Finite Fourier Series Approximation of Pseudoequinoctial Elements. International Journal of Aerospace Engineering No. 2019 (2019), pp.1-18.
https://search.emarefa.net/detail/BIM-1156118
نمط استشهاد الجمعية الطبية الأمريكية (AMA)
Zhou, Wanmeng& Li, Haiyang& Wang, Hua& Ding, Ran. Low-Thrust Trajectory Design Using Finite Fourier Series Approximation of Pseudoequinoctial Elements. International Journal of Aerospace Engineering. 2019. Vol. 2019, no. 2019, pp.1-18.
https://search.emarefa.net/detail/BIM-1156118
نوع البيانات
مقالات
لغة النص
الإنجليزية
الملاحظات
Includes bibliographical references
رقم السجل
BIM-1156118
قاعدة معامل التأثير والاستشهادات المرجعية العربي "ارسيف Arcif"
أضخم قاعدة بيانات عربية للاستشهادات المرجعية للمجلات العلمية المحكمة الصادرة في العالم العربي
تقوم هذه الخدمة بالتحقق من التشابه أو الانتحال في الأبحاث والمقالات العلمية والأطروحات الجامعية والكتب والأبحاث باللغة العربية، وتحديد درجة التشابه أو أصالة الأعمال البحثية وحماية ملكيتها الفكرية. تعرف اكثر