发明名称 |
SPACECRAFT WITH AERODYNAMIC CONTROL |
摘要 |
A spacecraft operating in a low earth orbit having an altitude in the range of 160 to 800 km has a main body that includes heat dissipating electrical equipment and an earth-facing payload. Control surfaces on the spacecraft are articulated so as to: provide three-axis attitude control to the spacecraft main body using aerodynamic drag effects, such that the earth-facing payload is maintained in a selected orientation with respect to the earth; and control one or both of orbit altitude and period by articulating the control surfaces so as to regulate an amount of aerodynamic drag. The control surfaces include a first control surface disposed, in an on-orbit configuration, on a boom, the boom being mechanically coupled with the main body, and with one or both of a solar array electrically coupled with the electrical equipment and a thermal radiating array thermally coupled with the electrical equipment. |
申请公布号 |
US2016244189(A1) |
申请公布日期 |
2016.08.25 |
申请号 |
US201514627936 |
申请日期 |
2015.02.20 |
申请人 |
Space Systems/Loral, LLC |
发明人 |
Turner Andrew E. |
分类号 |
B64G1/24 |
主分类号 |
B64G1/24 |
代理机构 |
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代理人 |
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主权项 |
1. A method comprising:
operating a spacecraft in a low earth orbit having an altitude in the range of 160 to 80 km, the spacecraft having a main body that includes heat dissipating electrical equipment and an earth-facing payload; articulating control surfaces so as to:
provide three-axis attitude control to the spacecraft main body using aerodynamic drag effects, such that the earth-facing payload is maintained in a selected orientation with respect to the earth; andcontrolling one or both of orbit altitude and period by articulating the control surfaces so as to regulate an amount of aerodynamic drag; wherein:
the control surfaces include a first control surface disposed, in an on-orbit configuration, on a boom, the boom being mechanically coupled with the main body, and with one or both of a solar array electrically coupled with the electrical equipment and a thermal radiating array thermally coupled with the electrical equipment. |
地址 |
Palo Alto CA US |