AU2019700A - Fast resonance shifting as a way to reduce propellant for space mission applications - Google Patents
Fast resonance shifting as a way to reduce propellant for space mission applicationsInfo
- Publication number
- AU2019700A AU2019700A AU20197/00A AU2019700A AU2019700A AU 2019700 A AU2019700 A AU 2019700A AU 20197/00 A AU20197/00 A AU 20197/00A AU 2019700 A AU2019700 A AU 2019700A AU 2019700 A AU2019700 A AU 2019700A
- Authority
- AU
- Australia
- Prior art keywords
- way
- space mission
- mission applications
- reduce propellant
- fast resonance
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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
- B64G1/244—Spacecraft control systems
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Navigation (AREA)
- Radio Relay Systems (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US8763698P | 1998-06-02 | 1998-06-02 | |
| US60087636 | 1998-06-02 | ||
| PCT/US1999/012213 WO2000013971A2 (en) | 1998-06-02 | 1999-06-02 | Fast resonance shifting as a way to reduce propellant for space mission applications |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| AU2019700A true AU2019700A (en) | 2000-03-27 |
Family
ID=22206354
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU20197/00A Abandoned AU2019700A (en) | 1998-06-02 | 1999-06-02 | Fast resonance shifting as a way to reduce propellant for space mission applications |
Country Status (2)
| Country | Link |
|---|---|
| AU (1) | AU2019700A (en) |
| WO (1) | WO2000013971A2 (en) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7869948B2 (en) * | 2007-04-27 | 2011-01-11 | Sirf Technology, Inc. | Method and apparatus in positioning without broadcast ephemeris |
| US8260540B2 (en) | 2007-04-27 | 2012-09-04 | Sirf Technology, Inc. | Systems and methods of communication in an assisted navigation system |
| FR2933671B1 (en) * | 2008-07-08 | 2010-12-17 | Thales Sa | METHOD FOR ALLEVING THE FUEL MASS ONBOARD AT AN INTERPLANETARY MISSION |
| RU2614464C2 (en) * | 2015-09-15 | 2017-03-28 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Spacecraft control method for flying around moon |
| RU2614446C2 (en) * | 2015-09-15 | 2017-03-28 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Spacecraft control method for flying around moon |
| RU2734705C1 (en) * | 2020-01-21 | 2020-10-22 | Публичное акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королёва" | Spacecraft control method during flight to moon |
| US11987396B2 (en) * | 2020-06-28 | 2024-05-21 | Mitsubishi Electric Research Laboratories Inc. | Fail-safe vehicle rendezvous in case of total control failure |
| US11807404B2 (en) * | 2020-06-28 | 2023-11-07 | Mitsubishi Electric Research Laboratories Inc. | Abort-safe vehicle rendezvous in case of partial control failure |
| CN116131898A (en) * | 2022-06-10 | 2023-05-16 | 北京大学 | Low-orbit satellite link frequency hopping communication method and system |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4580747A (en) * | 1983-03-15 | 1986-04-08 | Jerome Pearson | Method and apparatus for orbital plane changing |
| US4657211A (en) * | 1984-11-20 | 1987-04-14 | Rca Corporation | Spacecraft to shuttle docking method and apparatus |
| US4664344A (en) * | 1985-11-07 | 1987-05-12 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Apparatus and method of capturing an orbiting spacecraft |
| US4898349A (en) * | 1988-12-09 | 1990-02-06 | General Electric Company | Spacecraft approach/separation by use of angular measurement |
| US5158249A (en) * | 1990-10-12 | 1992-10-27 | Ball Corporation | Orbital systems for cislunar travel |
| US5806802A (en) * | 1993-11-12 | 1998-09-15 | Scott; David D. | Apparatus and methods for in-space satellite operations |
| US5511748A (en) * | 1993-11-12 | 1996-04-30 | Scott; David R. | Method for extending the useful life of a space satellite |
| US5813634A (en) * | 1995-10-23 | 1998-09-29 | Motorola, Inc. | Method for replacing failing satellites in a satellite communication system |
| JP3867315B2 (en) * | 1996-04-22 | 2007-01-10 | 三菱電機株式会社 | Automatic collision avoidance device |
-
1999
- 1999-06-02 AU AU20197/00A patent/AU2019700A/en not_active Abandoned
- 1999-06-02 WO PCT/US1999/012213 patent/WO2000013971A2/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| WO2000013971A3 (en) | 2000-07-06 |
| WO2000013971A9 (en) | 2000-10-05 |
| WO2000013971A2 (en) | 2000-03-16 |
| WO2000013971B1 (en) | 2000-11-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MK6 | Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase |