JPH0431700U - - Google Patents

Info

Publication number
JPH0431700U
JPH0431700U JP7459190U JP7459190U JPH0431700U JP H0431700 U JPH0431700 U JP H0431700U JP 7459190 U JP7459190 U JP 7459190U JP 7459190 U JP7459190 U JP 7459190U JP H0431700 U JPH0431700 U JP H0431700U
Authority
JP
Japan
Prior art keywords
control
accelerometer
amount
solar radiation
thruster
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.)
Pending
Application number
JP7459190U
Other languages
English (en)
Japanese (ja)
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 filed Critical
Priority to JP7459190U priority Critical patent/JPH0431700U/ja
Publication of JPH0431700U publication Critical patent/JPH0431700U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
JP7459190U 1990-07-13 1990-07-13 Pending JPH0431700U (US20020193084A1-20021219-M00002.png)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7459190U JPH0431700U (US20020193084A1-20021219-M00002.png) 1990-07-13 1990-07-13

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7459190U JPH0431700U (US20020193084A1-20021219-M00002.png) 1990-07-13 1990-07-13

Publications (1)

Publication Number Publication Date
JPH0431700U true JPH0431700U (US20020193084A1-20021219-M00002.png) 1992-03-13

Family

ID=31614413

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7459190U Pending JPH0431700U (US20020193084A1-20021219-M00002.png) 1990-07-13 1990-07-13

Country Status (1)

Country Link
JP (1) JPH0431700U (US20020193084A1-20021219-M00002.png)

Similar Documents

Publication Publication Date Title
Betts et al. Optimal low thrust trajectories to the moon
JPS6047159B2 (ja) 衛星の姿勢制御装置
JPH0655599B2 (ja) 3軸制御宇宙船をスピンアツプするための方法
EP1024082A3 (en) Combined stationkeeping and momentum management
JPH0133400B2 (US20020193084A1-20021219-M00002.png)
Ingoldby Guidance and control system design of the Viking planetary lander
JP2001240000A (ja) リアクションホイールを使用した機載姿勢制御
JPS61287899A (ja) 静止衛星の章動の制御方法および装置
JPH0431700U (US20020193084A1-20021219-M00002.png)
Reijneveld et al. Attitude control system of the Delfi-n3Xt satellite
FR2373823A1 (fr) Procede et dispositif de commande d'attitude de vehicule spatial
Song et al. A lunar cargo mission design strategy using variable low thrust
KR100778098B1 (ko) 인공위성 3축 자세제어용 제어 모멘트 자이로 클러스터
Cherry A UNIFIED EXPLICIT TECHNIQUE FOR PERFORMING ORBITAL INSERTION, SOFT LANDING, AND RENDEZVOUS WITH A THROT-TLEABLE ROCKET-PROPELLED SPACEVEHICLE
Kuhns et al. Singularity avoidance control laws for a multiple CMG spacecraft attitude control system
Regnier et al. Aocs design for scientific missions rosetta/mars express
BAKER Jr Application of astronomical perturbation techniques to the return of space vehicles
Williams et al. Trajectory issues affecting propulsion system sizing and operations of orbital inspection vehicles
Ikawa A unified three-dimensional trajectory simulation methodology
JPH0278499U (US20020193084A1-20021219-M00002.png)
Petersen et al. Satellite rendezvous navigational requirements
Thopil An attitude and orbit determination and control system for a small geostationary satellite
Chiarappa Analysis and design of space vehicle flight control systems. Volume VIII-Rendezvous and docking
Surauer et al. Attitude Control of Geostationary Satellites with Minimal Use of Gyros
DRAZNIN Problems in modeling a spin stabilized vehicle