CA2199436A1 - Controle au sol de l'orbite et de l'attitude d'un vaisseau spatial au moyen d'un circuit logique de selection de propulseurs a anticipation et de generateurs de couples magnetiques - Google Patents

Controle au sol de l'orbite et de l'attitude d'un vaisseau spatial au moyen d'un circuit logique de selection de propulseurs a anticipation et de generateurs de couples magnetiques

Info

Publication number
CA2199436A1
CA2199436A1 CA 2199436 CA2199436A CA2199436A1 CA 2199436 A1 CA2199436 A1 CA 2199436A1 CA 2199436 CA2199436 CA 2199436 CA 2199436 A CA2199436 A CA 2199436A CA 2199436 A1 CA2199436 A1 CA 2199436A1
Authority
CA
Canada
Prior art keywords
spacecraft
ahead
look
attitude control
selection logic
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.)
Granted
Application number
CA 2199436
Other languages
English (en)
Other versions
CA2199436C (fr
Inventor
Marc Takahashi
Donald W. Gamble
Mark Mclaren
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Lanteris Space LLC
Original Assignee
Individual
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.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of CA2199436A1 publication Critical patent/CA2199436A1/fr
Application granted granted Critical
Publication of CA2199436C publication Critical patent/CA2199436C/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
CA 2199436 1996-03-08 1997-03-07 Controle au sol de l'orbite et de l'attitude d'un vaisseau spatial au moyen d'un circuit logique de selection de propulseurs a anticipation et de generateurs de couples magnetiques Expired - Fee Related CA2199436C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US1303896P 1996-03-08 1996-03-08
US60/013,038 1996-03-08

Publications (2)

Publication Number Publication Date
CA2199436A1 true CA2199436A1 (fr) 1997-09-08
CA2199436C CA2199436C (fr) 2003-05-13

Family

ID=21757994

Family Applications (1)

Application Number Title Priority Date Filing Date
CA 2199436 Expired - Fee Related CA2199436C (fr) 1996-03-08 1997-03-07 Controle au sol de l'orbite et de l'attitude d'un vaisseau spatial au moyen d'un circuit logique de selection de propulseurs a anticipation et de generateurs de couples magnetiques

Country Status (2)

Country Link
JP (1) JPH101099A (fr)
CA (1) CA2199436C (fr)

Also Published As

Publication number Publication date
JPH101099A (ja) 1998-01-06
CA2199436C (fr) 2003-05-13

Similar Documents

Publication Publication Date Title
US5961077A (en) Method and a system for launching satellites simultaneously on non-coplanar orbits by using highly eccentric orbits and atmospheric braking
US5813633A (en) Method and apparatus for stationkeeping a satellite offset by pitch rotation
US6059233A (en) Method and a system for launching satellites on non-coplanar orbits, making the use of gravitational assistance from the moon
US6213432B1 (en) Method and a system for putting a space vehicle into orbit, using thrusters of high specific impulse
US6135394A (en) Practical method and apparatus for satellite stationkeeping
JP3934153B2 (ja) 宇宙内人工衛星の操作装置および方法
US5020746A (en) Method for satellite station keeping
US5803407A (en) Apparatus and methods for in-space satellite operations
EP0225683B1 (fr) Méthode pour accélérer le spin d'un vaisseau spatial contrôlable en direction de trois axes
US5507454A (en) Satellite and method to place this satellite in orbit by gravitational assistance
EP0602668B1 (fr) Procédé d'immobilisation de propergol
US5395076A (en) Spacecraft velocity change maneuvers by variable arcjets
US5931419A (en) Reducing satellite weight and cost
Marcuccio et al. Attitude and orbit control of small satellites and constellations with feep thrusters
US5568904A (en) Steered perigee velocity augmentation
EP0780300B1 (fr) Système double aux moitiés et configuration de propulseurs de contrôle à possée à couple intégral pour véhicule spatial stabilisé selon trois axes
Uesugi et al. MUSES-A double lunar swingby mission
Bentley et al. Syncom satellite program
Evans et al. Mission design of the Orbcomm constellation
Geffroy Optimal use of electric propulsion for future leo constellations positioning
Markland Attitude and orbit control for satellite broadcasting missions
Baker et al. Adaptation of the Olympus AOCS for use in Low Earth Orbit
POLLE Control of large Earth observation spacecrafts from SPOT 1 to PPF 1
Pocha Transfer Orbit
COVAULT Tight pace challenges Solar Max repair

Legal Events

Date Code Title Description
EEER Examination request
MKLA Lapsed