WO2004098994A3 - Attitude determination and control system for a solar sail spacecraft - Google Patents
Attitude determination and control system for a solar sail spacecraft Download PDFInfo
- Publication number
- WO2004098994A3 WO2004098994A3 PCT/US2003/040100 US0340100W WO2004098994A3 WO 2004098994 A3 WO2004098994 A3 WO 2004098994A3 US 0340100 W US0340100 W US 0340100W WO 2004098994 A3 WO2004098994 A3 WO 2004098994A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- solar sail
- control system
- attitude determination
- sail spacecraft
- spacecraft
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/407—Solar sailing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/405—Ion or plasma engines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/411—Electric propulsion
- B64G1/415—Arcjets or resistojets
Abstract
A solar sail spacecraft with microthrusters (21) approximate edges of the solar sail (11). The microthrusters provide attitude control and are mounted along spars (17). Some embodiments include control vanes (37).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US43305302P | 2002-12-13 | 2002-12-13 | |
US60/433,053 | 2002-12-13 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2004098994A2 WO2004098994A2 (en) | 2004-11-18 |
WO2004098994A3 true WO2004098994A3 (en) | 2005-02-10 |
Family
ID=33434862
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2003/040100 WO2004098994A2 (en) | 2002-12-13 | 2003-12-15 | Attitude determination and control system for a solar sail spacecraft |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2004098994A2 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE530415C2 (en) | 2006-09-04 | 2008-05-27 | Nanospace Ab | Gastrustor |
CN106339002B (en) * | 2016-10-14 | 2019-01-18 | 南京理工大学 | A kind of control of Solar sail spacecraft three-axis attitude and implementation method |
CN112340066B (en) * | 2020-11-23 | 2022-04-19 | 中国人民解放军国防科技大学 | Formula of can throwing solar sail spacecraft |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6194790B1 (en) * | 1999-11-22 | 2001-02-27 | The United States Of America As Represented By The Secretary Of The Air Force | Solar sail for power generation |
US20020116877A1 (en) * | 2001-02-28 | 2002-08-29 | Elmar Breitbach | Apparatus including a boom to be compressed and rolled up |
US20030010869A1 (en) * | 2001-07-16 | 2003-01-16 | Junichiro Kawaguchi | Large membrane space structure and method for its deployment and expansion |
-
2003
- 2003-12-15 WO PCT/US2003/040100 patent/WO2004098994A2/en not_active Application Discontinuation
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6194790B1 (en) * | 1999-11-22 | 2001-02-27 | The United States Of America As Represented By The Secretary Of The Air Force | Solar sail for power generation |
US20020116877A1 (en) * | 2001-02-28 | 2002-08-29 | Elmar Breitbach | Apparatus including a boom to be compressed and rolled up |
US20030010869A1 (en) * | 2001-07-16 | 2003-01-16 | Junichiro Kawaguchi | Large membrane space structure and method for its deployment and expansion |
Also Published As
Publication number | Publication date |
---|---|
WO2004098994A2 (en) | 2004-11-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AU1533799A (en) | Airfoils for wind turbine | |
AU2471200A (en) | Aircraft with removable structural payload module | |
AU5768598A (en) | Turbojet pod with laminar flow | |
AU2002312037A1 (en) | The use of aerodynamic forces to assist in the control and positioning of aircraft control surfaces and variable geometry systems | |
AU2251500A (en) | Gyrostabilized self propelled aircraft | |
AU1389695A (en) | Boundary layer control in aerodynamic low drag structures | |
AU3633701A (en) | Aircraft attitude sensor and feedback control system | |
AU3483895A (en) | Aircraft with jet flap propulsion | |
AU7819498A (en) | Reducing handwriting recognizer errors using decision trees | |
AU661994B2 (en) | Airfoil sail | |
WO2003049959A3 (en) | Multimodal, deployable vehicle | |
WO2000012269A3 (en) | Moment control unit for spacecraft attitude control | |
AU4223597A (en) | Wind turbine mounted on buoyant wing kite | |
AU2756900A (en) | Variable flexible stringer, bodyboard and method | |
WO2004098994A3 (en) | Attitude determination and control system for a solar sail spacecraft | |
AU2000300A (en) | Aircraft equipped with a bulky body causing an aerostatic thrust, and carrying wings | |
AU5061200A (en) | Method on regulating the air flow around the windmill wing and device for use insuch method | |
WO2001013525A3 (en) | Constellation of elliptical orbit satellites with line of apsides lying in or near the equatorial plane | |
AU2002227867A1 (en) | Aerodynamic wing with at least partially variable curvature and structural joints | |
FR2794254B1 (en) | POSITION CONTROL IN THREE SATELLITE AXES WITH LOW ALTITUDE | |
AU2003221806A1 (en) | Satellite energy and attitude control system | |
AU4569300A (en) | Hinged rigid sail with aerodynamic profile | |
AU2003276441A1 (en) | Control systems for use with flying craft and other remote elements | |
AU7492798A (en) | Cooling systems suitable for use with gas turbines | |
AU5809300A (en) | Lighter-than-air flying craft and method for counterbalancing the flying craft and for setting down load fastened to the same |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AK | Designated states |
Kind code of ref document: A2 Designated state(s): CA JP US |
|
AL | Designated countries for regional patents |
Kind code of ref document: A2 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LU MC NL PT RO SE SI SK TR |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
122 | Ep: pct application non-entry in european phase | ||
NENP | Non-entry into the national phase |
Ref country code: JP |
|
WWW | Wipo information: withdrawn in national office |
Country of ref document: JP |