JPH0474196U - - Google Patents

Info

Publication number
JPH0474196U
JPH0474196U JP11830890U JP11830890U JPH0474196U JP H0474196 U JPH0474196 U JP H0474196U JP 11830890 U JP11830890 U JP 11830890U JP 11830890 U JP11830890 U JP 11830890U JP H0474196 U JPH0474196 U JP H0474196U
Authority
JP
Japan
Prior art keywords
disturbance torque
spacecraft
attitude
flying
center
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
JP11830890U
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 JP11830890U priority Critical patent/JPH0474196U/ja
Publication of JPH0474196U publication Critical patent/JPH0474196U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
JP11830890U 1990-11-09 1990-11-09 Pending JPH0474196U (en])

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11830890U JPH0474196U (en]) 1990-11-09 1990-11-09

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11830890U JPH0474196U (en]) 1990-11-09 1990-11-09

Publications (1)

Publication Number Publication Date
JPH0474196U true JPH0474196U (en]) 1992-06-29

Family

ID=31866227

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11830890U Pending JPH0474196U (en]) 1990-11-09 1990-11-09

Country Status (1)

Country Link
JP (1) JPH0474196U (en])

Similar Documents

Publication Publication Date Title
Wiśniewski et al. Fully magnetic attitude control for spacecraft subject to gravity gradient
CN106660641B (zh) 控制卫星在地球轨道中的轨道的方法、卫星和控制这种卫星的轨道的系统
US6053455A (en) Spacecraft attitude control system using low thrust thrusters
CN110304279B (zh) 一种电推进卫星的质心在轨标定补偿方法
JPH0624397A (ja) ジンバルおよび絞り調整されるスラスタを使用する宇宙船姿勢制御および運動量アンローディング方法および装置
JPH0655599B2 (ja) ３軸制御宇宙船をスピンアツプするための方法
JP2001240000A (ja) リアクションホイールを使用した機載姿勢制御
US5957411A (en) Method using double thruster firings to deadbeat flexible solar array structural oscillations
US12263962B2 (en) Momentum wheels and reaction wheels for objects in space
CN114706413A (zh) 近地轨道微纳卫星变质心姿态控制方法及系统
US10029807B2 (en) Spacecraft and orbital plane change method therefor
Barinova et al. Determining of equilibrium positions of CubeSat nanosatellite under the influence of aerodynamic and gravitational moments
JPH0474196U (en])
Hima et al. Motion generation on trim trajectories for an autonomous underactuated airship
Gobiha et al. Autonomous maneuvering of a stratospheric airship
Reijneveld et al. Attitude control system of the Delfi-n3Xt satellite
US20060038080A1 (en) Solar control method for spacecraft
Wisniewski et al. Three-axis satellite attitude control based on magnetic torquing
Song et al. ESO-based robust predictive control of lunar module with fuel sloshing dynamics
Mohammed et al. Magnetorquer control for orbital manoeuvre of low earth orbit microsatellite
LEBSOCK et al. Double gimballed reaction wheel attitude control system for high altitude communications satellites
CN120003724A (zh) 一种适用于多载荷一体化的多体卫星构型
Azor Solar attitude control including active nutation damping in a fixed-momentum wheel satellite
CN115203830A (zh) 一种再入临近空间气动大异面轨道重构方法
Parvez et al. Low-thrust insertion into orbit around Mars