2023
DOI: 10.1016/j.asr.2022.10.015
|View full text |Cite
|
Sign up to set email alerts
|

Attitude control actuator scaling laws for orbiting solar reflectors

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
4
1

Citation Types

0
5
0

Year Published

2023
2023
2024
2024

Publication Types

Select...
5
1

Relationship

0
6

Authors

Journals

citations
Cited by 7 publications
(5 citation statements)
references
References 22 publications
0
5
0
Order By: Relevance
“…Quantum dot solar cells are an upcoming technological advancement that uses semiconductor particles called quantum dots to absorb and convert solar energy into electrical power. The capability to change the band gaps of quantum dots enables exact modification of their light absorption characteristics, hence increasing their capacity in collecting light energy [14]. Quantum dot solar cells demonstrate considerable potential in achieving substantial levels of energy conversion efficiency.…”
Section: Solar Energy Technologiesmentioning
confidence: 99%
“…Quantum dot solar cells are an upcoming technological advancement that uses semiconductor particles called quantum dots to absorb and convert solar energy into electrical power. The capability to change the band gaps of quantum dots enables exact modification of their light absorption characteristics, hence increasing their capacity in collecting light energy [14]. Quantum dot solar cells demonstrate considerable potential in achieving substantial levels of energy conversion efficiency.…”
Section: Solar Energy Technologiesmentioning
confidence: 99%
“…Figure 5 illustrates the peak angular acceleration required during the tracking (black line) and reorientation (blue line) phases as a function of the orbit altitude (see Ref. [34] for additional details). Also shown are the equivalent gravity gradient and solar radiation pressure peak angular accelerations.…”
Section: Reflector Attitude Controlmentioning
confidence: 99%
“…Alternatively, as proposed in Ref. [34], a pair of CMGs could be appended at the top of two booms normal to the reflector, as shown in Fig 6 . It can be shown that if the wheel mass is 1/24 of the reflector mass (neglecting the boom mass), the inertia of the reflector about the three Fig. 5.…”
Section: Reflector Attitude Controlmentioning
confidence: 99%
See 2 more Smart Citations