[an error occurred while processing this directive]
   
 
���¿��ټ��� �߼�����
   ��ҳ  �ڿ�����  ��ί��  Ͷ��ָ��  �ڿ�����  ��������  �� �� ��  ��ϵ����
�������պ����ѧѧ�� 2008, Vol. 34 Issue (05) :529-532    DOI:
���� ����Ŀ¼ | ����Ŀ¼ | ������� | �߼����� << | >>
�Եع۲��������������ѧ���Ż�
̷����1, �ӱ���1, ������2, �ƺ�2*
1. ��������ҵ��ѧ ����ѧԺ, ������ 150001;
2. �������պ����ѧ �ѧԺ, ���� 100083
Multidisciplinary optimization in earth observation satellite main parameters
Tan Chunlin1, Pang Baojun1, Zhang Lingyan2, Huang Hai2*
1. School of Astronautics, Harbin Institute of Technology, Harbin 150001, China;
2. School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

ժҪ
�����
�������
Download: PDF (365KB)   HTML 1KB   Export: BibTeX or EndNote (RIS)      Supporting Info
ժҪ ��ԶԵع۲�������������������,�������ԶԵع۲��������ΪĿ��Ķ�ѧ���Ż�ģ��,�����˹���ơ���Դ���ṹ���ƽ�����Ч�غ�5����ϵͳ����Ʊ�������ӦԼ������,���������ػ����������Ƶ�Լ������,ͨ�����鹫ʽ��������ģ��.����Эͬ�Ż�����,������㷣��������ϵͳ���Ż�����ת��Ϊ��Լ���Ż������Ը���Эͬ�Ż�ϵͳ������ֵȱ��,�����˶�ѧ������Ż����.����������ͨ���Ż����������ǵĶԵع۲�����,��֤�˸÷����ĺ�����.��ģ˼·���Ż������������ڸ����Ϲ���ʵ�ʵ����Dz������.
Service
�ѱ����Ƽ�������
�����ҵ����
�������ù�����
Email Alert
RSS
�����������
̷����
�ӱ���
������
�ƺ�
�ؼ����� �Եع۲�����   ���   �Ż�     
Abstract�� A model of multidisciplinary design optimization (MDO) was established for the system parameter design problem of an earth observation satellite. It takes the observation performance as the objective of optimization, while the design variables and constraints are dealt with five main subsystems including attitude and orbit control, power, structures, propulsion, payload, besides constraints made by launch vehicle and the analysis modules modeled by empirical formula. A multidisciplinary design optimization framework was established by using the collaborative optimization (CO) method, and exterior penalty technique was using to change the constrained question into an unconstrained question during system level optimization, so as to improve numerical difficulties in CO method application. The results show that the earth observation performance can be improved by this optimization method and the method was efficient. The modeling and optimization method of the work can be expected to apply to practical engineering satellite parameters design.
Keywords�� earth observation satellites   design   optimization     
Received 2007-05-08;
Fund:

���춫�����������޹�˾Ԥ��������Ŀ

About author: ̷����(1967-),��,����������,��ʿ��,tanchlin@yahoo.com.
���ñ���:   
̷����, �ӱ���, ������, �ƺ�.�Եع۲��������������ѧ���Ż�[J]  �������պ����ѧѧ��, 2008,V34(05): 529-532
Tan Chunlin, Pang Baojun, Zhang Lingyan, Huang Hai.Multidisciplinary optimization in earth observation satellite main parameters[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2008,V34(05): 529-532
���ӱ���:  
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2008/V34/I05/529
Copyright 2010 by �������պ����ѧѧ��