JPH0370609U - - Google Patents

Info

Publication number
JPH0370609U
JPH0370609U JP12958989U JP12958989U JPH0370609U JP H0370609 U JPH0370609 U JP H0370609U JP 12958989 U JP12958989 U JP 12958989U JP 12958989 U JP12958989 U JP 12958989U JP H0370609 U JPH0370609 U JP H0370609U
Authority
JP
Japan
Prior art keywords
navigation guidance
spacecraft
control
trajectory
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
JP12958989U
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 JP12958989U priority Critical patent/JPH0370609U/ja
Publication of JPH0370609U publication Critical patent/JPH0370609U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
JP12958989U 1989-11-06 1989-11-06 Pending JPH0370609U (OSRAM)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12958989U JPH0370609U (OSRAM) 1989-11-06 1989-11-06

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12958989U JPH0370609U (OSRAM) 1989-11-06 1989-11-06

Publications (1)

Publication Number Publication Date
JPH0370609U true JPH0370609U (OSRAM) 1991-07-16

Family

ID=31677208

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12958989U Pending JPH0370609U (OSRAM) 1989-11-06 1989-11-06

Country Status (1)

Country Link
JP (1) JPH0370609U (OSRAM)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021015351A (ja) * 2019-07-10 2021-02-12 国立研究開発法人宇宙航空研究開発機構 誘導プログラム、誘導方法、及び誘導装置

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021015351A (ja) * 2019-07-10 2021-02-12 国立研究開発法人宇宙航空研究開発機構 誘導プログラム、誘導方法、及び誘導装置

Similar Documents

Publication Publication Date Title
EP0225683A1 (en) Method for spinning up a three-axis controlled spacecraft
JPS6047159B2 (ja) 衛星の姿勢制御装置
US3547381A (en) Three-axis orientation system
CA2032267A1 (en) Lightweight missile guidance system
US4807835A (en) Spacecraft attitude stabilization system
JPH0370609U (OSRAM)
EP1311428B1 (en) Employing booster trajectory in a payload inertial measurement unit
US4044237A (en) Missile maneuver concept
FR2373823A1 (fr) Procede et dispositif de commande d'attitude de vehicule spatial
Garner Simulator studies of simple attitude control for spin-stabilized vehicles
JPS63290400A (ja) 双操舵型飛しょう体の操舵方法
JPS62125895U (OSRAM)
JPH0437838Y2 (OSRAM)
JPH0346796U (OSRAM)
JPH0190699U (OSRAM)
JPS5863200U (ja) 人工衛星の三軸姿勢制御装置
HALYO Development of an optimal automatic control law and filter algorithm for steep glideslope capture and glideslope tracking[Final Report]
JPS63173800A (ja) デユアルスピンタ−ン方式
JPS5976898U (ja) 飛しよう体誘導装置
JPH08310500A (ja) 軌道制御装置
JPS62227899A (ja) 人工衛星の姿勢制御方式
GUSTAFSON et al. Nonlinear control theory for missile autopilot design(Final Technical Report, 15 Aug. 1986- 14 Feb.)(1987)
JPH0157999U (OSRAM)
IT1102670B (it) Perfezionamento nei sistemi di gui da per veicoli
JPH03112680U (OSRAM)