DE3587199D1 - Kollimationskompensiersystem fuer raumfahrzeuginstrumente. - Google Patents

Kollimationskompensiersystem fuer raumfahrzeuginstrumente.

Info

Publication number
DE3587199D1
DE3587199D1 DE8585905949T DE3587199T DE3587199D1 DE 3587199 D1 DE3587199 D1 DE 3587199D1 DE 8585905949 T DE8585905949 T DE 8585905949T DE 3587199 T DE3587199 T DE 3587199T DE 3587199 D1 DE3587199 D1 DE 3587199D1
Authority
DE
Germany
Prior art keywords
instrument
motion
spacecraft
collimation
compensation system
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 - Fee Related
Application number
DE8585905949T
Other languages
English (en)
Other versions
DE3587199T2 (de
Inventor
T Plescia
W Gamble
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.)
Space Systems Loral LLC
Original Assignee
Loral Space Systems Inc
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 Loral Space Systems Inc filed Critical Loral Space Systems Inc
Publication of DE3587199D1 publication Critical patent/DE3587199D1/de
Application granted granted Critical
Publication of DE3587199T2 publication Critical patent/DE3587199T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/12—Supports; Mounting means
    • H01Q1/18—Means for stabilising antennas on an unstable platform
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE8585905949T 1985-09-30 1985-09-30 Kollimationskompensiersystem fuer raumfahrzeuginstrumente. Expired - Fee Related DE3587199T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US1985/001887 WO1987002145A1 (en) 1985-09-30 1985-09-30 Pointing compensation system for spacecraft instruments

Publications (2)

Publication Number Publication Date
DE3587199D1 true DE3587199D1 (de) 1993-04-22
DE3587199T2 DE3587199T2 (de) 1993-08-05

Family

ID=22188864

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8585905949T Expired - Fee Related DE3587199T2 (de) 1985-09-30 1985-09-30 Kollimationskompensiersystem fuer raumfahrzeuginstrumente.

Country Status (5)

Country Link
EP (1) EP0246226B1 (de)
JP (1) JPS63500931A (de)
DE (1) DE3587199T2 (de)
IN (1) IN164849B (de)
WO (1) WO1987002145A1 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6393255B1 (en) * 1999-08-11 2002-05-21 Hughes Electronics Corp. Satellite antenna pointing system
CN105676671B (zh) * 2014-11-21 2018-05-15 上海新跃仪表厂 一种对日定向控制的半物理仿真测试系统

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4375878A (en) * 1980-10-28 1983-03-08 Lockheed Missiles & Space Company, Inc. Space satellite with agile payload orientation system
FR2502404A1 (fr) * 1981-03-20 1982-09-24 Matra Dispositif de montage articule, notamment d'un sous-ensemble de satellite artificiel
US4418350A (en) * 1981-03-23 1983-11-29 Hughes Aircraft Company Two-axis antenna direction control system
US4437047A (en) * 1981-07-13 1984-03-13 Hughes Aircraft Company System for autonomous earth-pointing acquisition of a dual-spin satellite
JPS5893699A (ja) * 1981-11-27 1983-06-03 三菱電機株式会社 飛しよう体の塔載機器回転装置
JPH07112840B2 (ja) * 1984-03-15 1995-12-06 三菱電機株式会社 人工衛星の姿勢およびアンテナ指向制御装置

Also Published As

Publication number Publication date
EP0246226A4 (en) 1990-12-12
JPS63500931A (ja) 1988-04-07
WO1987002145A1 (en) 1987-04-09
IN164849B (de) 1989-06-10
EP0246226B1 (de) 1993-03-17
EP0246226A1 (de) 1987-11-25
DE3587199T2 (de) 1993-08-05

Similar Documents

Publication Publication Date Title
Stolarski et al. The atmospheric effects of stratospheric aircraft: A third program report
DE3587199D1 (de) Kollimationskompensiersystem fuer raumfahrzeuginstrumente.
GB1116543A (en) Attitude computer with rotatable reference frame
DE3480882D1 (de) Elektronische steuerung eines matrixdruckers.
GB1160471A (en) An Acceleration Motion Simulator.
ATE98791T1 (de) Mikroprogrammablaufsteuerung.
ES2003719A6 (es) Dispositivo aeronautico para generar una triple redundancia para cuanto menos dos ejes en el espacio, en la estabilizacion y control de la orientacion de vuelo
JPS5630359A (en) Picture data transfer system
ZAZYKIN Possibilities of creating invariant man-machine systems[Abstract Only]
Caudill Mass-balance model for a controlled ecological life support system on Mars
JPS6421523A (en) Mouse
MATSUOKA Control design and performance evaluation for flexible manipulators(Ph. D. Thesis)
MEIROVITCH et al. Maneuvering of flexible spacecraft with application to SCOLE((Spacecraft Control Laboratory Experiment))
Rodden On Vibration and Flutter Analysis With Free-Free Boundary Conditions
Foley Control of a spacecraft using a reaction control system
Kargu Spacecraft attitude stabilization systems
Wargo et al. The UDOFT Flight Simulation System
Ivashkin Spaceflight mechanics
Poelaert et al. Analysis and design of an attitude control system for non-rigid satellites
Shin Spacecraft attitude control system test and evaluation.
Greipp A study of the effects of computer-assisted instruction on nursing graduates state board scores.
Erich et al. SIMSTAR missile simulation: A large scale example.
PITARYS Debugging distributed Ada avionics software
McMillan et al. Motion simulation with a G-seat system: Sensory and performance mechanisms
BILLINGSLEY Sting dynamics of wind tunnel models[Final Report, 1 Jul. 1974- 30 Jun. 1975]

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee