CA1041608A - Minimisation de la mutation residuelle d'un vaisseau spatial due a des couples perturbateurs - Google Patents

Minimisation de la mutation residuelle d'un vaisseau spatial due a des couples perturbateurs

Info

Publication number
CA1041608A
CA1041608A CA234,053A CA234053A CA1041608A CA 1041608 A CA1041608 A CA 1041608A CA 234053 A CA234053 A CA 234053A CA 1041608 A CA1041608 A CA 1041608A
Authority
CA
Canada
Prior art keywords
spacecraft
period
logic
nutation
generating means
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.)
Expired
Application number
CA234,053A
Other languages
English (en)
Inventor
Kevin J. Phillips
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.)
RCA Corp
Original Assignee
RCA Corp
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 RCA Corp filed Critical RCA Corp
Priority to CA234,053A priority Critical patent/CA1041608A/fr
Application granted granted Critical
Publication of CA1041608A publication Critical patent/CA1041608A/fr
Expired legal-status Critical Current

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
CA234,053A 1975-08-25 1975-08-25 Minimisation de la mutation residuelle d'un vaisseau spatial due a des couples perturbateurs Expired CA1041608A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA234,053A CA1041608A (fr) 1975-08-25 1975-08-25 Minimisation de la mutation residuelle d'un vaisseau spatial due a des couples perturbateurs

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA234,053A CA1041608A (fr) 1975-08-25 1975-08-25 Minimisation de la mutation residuelle d'un vaisseau spatial due a des couples perturbateurs

Publications (1)

Publication Number Publication Date
CA1041608A true CA1041608A (fr) 1978-10-31

Family

ID=4103882

Family Applications (1)

Application Number Title Priority Date Filing Date
CA234,053A Expired CA1041608A (fr) 1975-08-25 1975-08-25 Minimisation de la mutation residuelle d'un vaisseau spatial due a des couples perturbateurs

Country Status (1)

Country Link
CA (1) CA1041608A (fr)

Similar Documents

Publication Publication Date Title
EP0148550B1 (fr) Méthode et appareil pour le réglage transitoire de propulseurs
US3984071A (en) Satellite nutation attenuation apparatus
JP2001270499A (ja) スラスタ増強による磁気トルク発生器制御
EP0461394A1 (fr) Méthode d'orientation à pointage terrestre d'un véhicule spatial
JPH04293698A (ja) 3軸安定方式の人工衛星のための姿勢制御装置
US3977633A (en) Orientation system for a spin stabilized spacecraft
GB1478792A (en) Attitude control systems
US3073550A (en) Guidance system for missiles
US4193570A (en) Active nutation controller
US3547381A (en) Three-axis orientation system
EP0251692A2 (fr) Système de commande de l'orbite d'un satellite
US4504032A (en) Control of nutation in a spacecraft
US3830447A (en) Active nutation damping in dual-spin spacecraft
US4023752A (en) Elimination of residual spacecraft nutation due to propulsive torques
US3767139A (en) Spacecraft spin stabilization system
US4807835A (en) Spacecraft attitude stabilization system
US4142695A (en) Vehicle guidance system
US3997137A (en) Minimization of residual spacecraft nutation due to disturbing torques
CA1041608A (fr) Minimisation de la mutation residuelle d'un vaisseau spatial due a des couples perturbateurs
US4824052A (en) Nutation sensor and nutation control system for a dual-spin stabilized satellite
DOUGHERTY et al. Analysis and design of WHECON-An attitude control concept
US4560120A (en) Spin stabilized impulsively controlled missile (SSICM)
USRE30429E (en) Minimization of residual spacecraft nutation due to disturbing torques
US4591118A (en) Hysteresis conditioner for spacecraft attitude control
EP0187859A1 (fr) Satellite a rotation stabilisee avec sous-systeme de commande de la nutation