USB423441I5 - - Google Patents

Info

Publication number: USB423441I5
Authority: US; United States
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.): Pending

Application number

Priority date (The priority date 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 date listed.)

1973-12-10

Filing date

1973-12-10

Publication date

1976-02-17

1973-12-10 Application filed filed Critical

1973-12-10 Priority to US05/423,441 priority Critical patent/US3997137A/en

1976-02-17 Publication of USB423441I5 publication Critical patent/USB423441I5/en

1976-12-14 Application granted granted Critical

1976-12-14 Publication of US3997137A publication Critical patent/US3997137A/en

1993-12-14 Anticipated expiration legal-status Critical

Status Expired - Lifetime legal-status Critical Current

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
- B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
- 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
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/281—Spin-stabilised spacecraft

Landscapes

Engineering & Computer Science (AREA)
Remote Sensing (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)

US05/423,441 1973-12-10 1973-12-10 Minimization of residual spacecraft nutation due to disturbing torques Expired - Lifetime US3997137A (en)

Priority Applications (1)

Application Number	Priority Date	Filing Date	Title
US05/423,441 US3997137A (en)	1973-12-10	1973-12-10	Minimization of residual spacecraft nutation due to disturbing torques

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US05/423,441 US3997137A (en)	1973-12-10	1973-12-10	Minimization of residual spacecraft nutation due to disturbing torques

Related Child Applications (1)

Application Number	Title	Priority Date	Filing Date
US05/968,799 Reissue USRE30429E (en)	1978-12-12	1978-12-12	Minimization of residual spacecraft nutation due to disturbing torques

Publications (2)

Publication Number	Publication Date
USB423441I5 true USB423441I5 (en)	1976-02-17
US3997137A US3997137A (en)	1976-12-14

Family

ID=23678914

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
US05/423,441 Expired - Lifetime US3997137A (en)	1973-12-10	1973-12-10	Minimization of residual spacecraft nutation due to disturbing torques

Country Status (1)

Country	Link
US (1)	US3997137A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4825646A (en) *	1987-04-23	1989-05-02	Hughes Aircraft Company	Spacecraft with modulated thrust electrostatic ion thruster and associated method
US4931942A (en) *	1988-05-26	1990-06-05	Ford Aerospace Corporation	Transition control system for spacecraft attitude control
US5222023A (en) *	1991-04-02	1993-06-22	Space Systems/Loral, Inc.	Compensated transition for spacecraft attitude control
FR2993863B1 (en) *	2012-07-27	2014-08-29	Thales Sa	METHOD FOR REDUCING THE KINETIC MOMENT AND ATTITUDE CONTROL OF A SPATIAL MACHINE

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2974594A (en) *	1958-08-14	1961-03-14	Boehm Josef	Space vehicle attitude control system
US3135479A (en) *	1963-04-01	1964-06-02	Ryan Aeronautical Co	Method of reducing velocity vector angular error of a space vehicle when thrust is applied
US3384323A (en) *	1965-09-27	1968-05-21	Ltv Aerospace Corp	Attitude and coning control system for spin-stabilized vehicles
FR1468913A (en) *	1965-11-13	1967-02-10	Nord Aviation	Method and device for stabilizing, in a fixed direction, a slowly rotating vehicle
US3414214A (en) *	1966-05-31	1968-12-03	Trw Inc	Satellite positioning system
US3643897A (en) *	1968-10-18	1972-02-22	Communications Satellite Corp	Nutation correction system for spin-stabilized satellite
US3695554A (en) *	1970-10-16	1972-10-03	Rca Corp	Nutation damping in dual-spin spacecraft

1973
- 1973-12-10 US US05/423,441 patent/US3997137A/en not_active Expired - Lifetime

Also Published As

Publication number	Publication date
US3997137A (en)	1976-12-14

Publication	Publication Date	Title
AR201758A1 (en)	1975-04-15
AU476761B2 (en)	1976-09-30
AU465372B2 (en)	1975-09-25
AR201235Q (en)	1975-02-21
AR201231Q (en)	1975-02-21
AU474593B2 (en)	1976-07-29
AU474511B2 (en)	1976-07-22
AU474838B2 (en)	1976-08-05
AU471343B2 (en)	1976-04-15
AU465453B2 (en)	1975-09-25
AU465434B2 (en)	1975-09-25
AU450229B2 (en)	1974-07-04
AU476714B2 (en)	1976-09-30
AR201229Q (en)	1975-02-21
AU466283B2 (en)	1975-10-23
AU472848B2 (en)	1976-06-03
AU476696B2 (en)	1976-09-30
USB423441I5 (en)	1976-02-17
AU477823B2 (en)	1975-06-19
AU477824B2 (en)	1975-07-17
AU471461B2 (en)	1976-04-29
AR200885A1 (en)	1974-12-27
AR201432A1 (en)	1975-03-14
AR210729A1 (en)	1977-09-15
AU476873B1 (en)	1975-01-09