Near-minimum-fuel Strategy for Continuous Single-axis Maneuvers of a Rigid Body

被引：1

作者：

Kim, Donghoon ^{[1
]}

Leeghim, Henzeh ^{[2
]}

机构：

[1] Mississippi State Univ, Dept Aerosp Engn, Mississippi State, MS 39762 USA

[2] Chosun Univ, Dept Aerosp Engn, Gwangju 61452, South Korea

来源：

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 2019年 / 62卷 / 03期

关键词：

Near-minimum-fuel; Bang-off-bang Control; Smooth Function; Switch Time; Rest-to-rest; TIME;

D O I：

10.2322/tjsass.62.169

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

页码：169 / 172

页数：4

共 32 条

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Texas A&M Univ, College Station, United States
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ACTA ASTRONAUTICA, 2021, 180 : 527 - 537
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N. I. Amel’kin
Mechanics of Solids, 2009, 44 : 1 - 13
[8] SINGLE-AXIS SPACECRAFT ATTITUDE MANEUVERS USING AN OPTIMAL REACTION WHEEL POWER CRITERION
SKAAR, SB
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[9] Single-Axis, Spin-to-Spin Slew Maneuvers Under a Finite Jerk Constraint
Lee, Donghun
Song, Young-Joo
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2019, 42 (09) : 2116 - 2123
[10] Near minimum-time three dimensional maneuvers of rigid and flexible spacecraft
Bell, Mark J., 1600, American Astronautical Soc, San Diego (42):

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