Modified solution for finding the optimal angle of spacecraft walls under orbital debris impacts

被引：0

作者：

机构：

[1] Pantelides, Chris P.

[2] Tzan, Shyh-Rong

来源：

Pantelides, Chris P. | 1600年 / Publ by AIAA, Washington, DC, United States卷 / 31期

关键词：

Walls (structural partitions);

D O I：

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摘要：

引用

共 11 条

[1] MODIFIED SOLUTION FOR FINDING THE OPTIMAL ANGLE OF SPACECRAFT WALLS UNDER ORBITAL DEBRIS IMPACTS
PANTELIDES, CP
TZAN, SR
AIAA JOURNAL, 1993, 31 (06) : 1162 - 1165
[2] Spacecraft wall design for increased protection against penetration by orbital debris impacts
Schonberg, William P., 1600, (29):
[3] SPACECRAFT WALL DESIGN FOR INCREASED PROTECTION AGAINST PENETRATION BY ORBITAL DEBRIS IMPACTS
SCHONBERG, WP
TULLOS, RJ
AIAA JOURNAL, 1991, 29 (12) : 2207 - 2214
[4] Orbital debris impacts against spacecraft multiple shields: comparison of hypervelocity experiments and hydrocode simulations
Palmieri, D
Marchetti, M
Destefanis, R
Faraud, M
STRUCTURES UNDER SHOCK AND IMPACT V, 1998, 2 : 331 - 340
[5] Solution of a Problem of Spacecraft's Orbit Optimal Reorientation Using Quaternion Equations of Orbital System of Coordinates Orientation
Pankratov, I. A.
Sapunkov, Ya. G.
Chelnokov, Yu. N.
IZVESTIYA SARATOVSKOGO UNIVERSITETA NOVAYA SERIYA-MATEMATIKA MEKHANIKA INFORMATIKA, 2013, 13 (01): : 84 - 92
[6] An Alternate Method for Finding Optimal Solution to Solid Transportation Problem under Fuzzy Environment
Vidhya, V.
Ganesan, K.
3RD INTERNATIONAL CONFERENCE ON ADVANCES IN MECHANICAL ENGINEERING (ICAME 2020), PTS 1-6, 2020, 912
[7] Modified particle swarm optimisation with a novel initialisation for finding optimal solution to the transmission expansion planning problem
Murugan, P.
IET GENERATION TRANSMISSION & DISTRIBUTION, 2012, 6 (11) : 1132 - 1142
[8] Solution of the problem of the optimal turn of a spherically symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions
Molodenkov, AV
Sapunkov, YG
JOURNAL OF COMPUTER AND SYSTEMS SCIENCES INTERNATIONAL, 2004, 43 (02) : 317 - 328
[9] A solution of the optimal turn problem of an axially symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions
Molodenkov, A. V.
Sapunkov, Ya. G.
JOURNAL OF COMPUTER AND SYSTEMS SCIENCES INTERNATIONAL, 2007, 46 (02) : 310 - 323
[10] A solution of the optimal turn problem of an axially symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions
A. V. Molodenkov
Ya. G. Sapunkov
Journal of Computer and Systems Sciences International, 2007, 46 : 310 - 323

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