DE60003381D1 - Korrigierende Vorrichtung für Lagewinkelsensoren eines künstlichen Satellites - Google Patents

Korrigierende Vorrichtung für Lagewinkelsensoren eines künstlichen Satellites

Info

Publication number
DE60003381D1
DE60003381D1 DE60003381T DE60003381T DE60003381D1 DE 60003381 D1 DE60003381 D1 DE 60003381D1 DE 60003381 T DE60003381 T DE 60003381T DE 60003381 T DE60003381 T DE 60003381T DE 60003381 D1 DE60003381 D1 DE 60003381D1
Authority
DE
Germany
Prior art keywords
position angle
artificial satellite
angle sensors
corrective device
corrective
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 - Lifetime
Application number
DE60003381T
Other languages
English (en)
Other versions
DE60003381T2 (de
Inventor
Toshiaki Yamashita
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.)
NEC Corp
Original Assignee
NEC 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 NEC Corp filed Critical NEC Corp
Application granted granted Critical
Publication of DE60003381D1 publication Critical patent/DE60003381D1/de
Publication of DE60003381T2 publication Critical patent/DE60003381T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/365Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244Spacecraft control systems
    • B64G1/245Attitude control algorithms for spacecraft attitude control
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/10Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1021Earth observation satellites
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/66Arrangements or adaptations of apparatus or instruments, not otherwise provided for
DE60003381T 1999-12-10 2000-12-08 Korrigierende Vorrichtung für Lagewinkelsensoren eines künstlichen Satellites Expired - Lifetime DE60003381T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP35239799A JP3428539B2 (ja) 1999-12-10 1999-12-10 人工衛星の姿勢角センサ較正装置
JP35239799 1999-12-10

Publications (2)

Publication Number Publication Date
DE60003381D1 true DE60003381D1 (de) 2003-07-24
DE60003381T2 DE60003381T2 (de) 2004-05-19

Family

ID=18423798

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60003381T Expired - Lifetime DE60003381T2 (de) 1999-12-10 2000-12-08 Korrigierende Vorrichtung für Lagewinkelsensoren eines künstlichen Satellites

Country Status (4)

Country Link
US (1) US6336062B1 (de)
EP (1) EP1106505B1 (de)
JP (1) JP3428539B2 (de)
DE (1) DE60003381T2 (de)

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US7835826B1 (en) 2005-12-13 2010-11-16 Lockheed Martin Corporation Attitude determination system for yaw-steering spacecraft
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KR101017606B1 (ko) * 2008-12-22 2011-02-28 한국항공우주연구원 단일영상을 이용한 자세각센서 삼차원 오정렬 보정방법
US8212714B1 (en) * 2009-08-31 2012-07-03 Sandia Corporation Using doppler radar images to estimate aircraft navigational heading error
TWI403691B (zh) * 2009-09-08 2013-08-01 Nat Applied Res Laboratories The method of taking the telemetry instrument
CN103425134B (zh) * 2012-05-18 2016-08-17 宁波市鄞州麦谷农业科技有限公司 高速插秧机的卫星导航自动驾驶系统及其方法
KR101282718B1 (ko) * 2012-12-28 2013-07-05 한국항공우주연구원 선형배열 영상센서와 자세제어 센서 간의 절대 오정렬 보정방법
US9251419B2 (en) 2013-02-07 2016-02-02 Digitalglobe, Inc. Automated metric information network
CN103148870B (zh) * 2013-03-01 2015-07-08 国家测绘地理信息局卫星测绘应用中心 基于高精度配准控制点的卫星ccd阵列影像几何检校方法
JP6066940B2 (ja) * 2014-01-30 2017-01-25 三菱電機株式会社 画像ナビゲーション装置、衛星および画像ナビゲーション方法
CN105628051B (zh) * 2014-10-29 2018-08-21 北京临近空间飞行器系统工程研究所 一种嵌入式大气测量装置性能评估方法
CN104501836B (zh) * 2014-12-22 2018-01-05 中国人民解放军海军航空工程学院青岛校区 一种用于飞参数据标校的无线装置
CN104807477B (zh) * 2015-04-24 2017-10-17 国家测绘地理信息局卫星测绘应用中心 一种基于靶标控制点的卫星ccd阵列影像几何检校方法
CN104848860B (zh) * 2015-05-19 2017-11-07 北京空间飞行器总体设计部 一种敏捷卫星成像过程姿态机动规划方法
CN105136164B (zh) * 2015-08-13 2019-04-05 航天恒星科技有限公司 考虑卫星综合运动的凝视成像仿真及质量评估方法及装置
CN105160125B (zh) * 2015-09-24 2018-09-18 航天东方红卫星有限公司 一种星敏感器四元数的仿真分析方法
CN105424047B (zh) * 2015-10-30 2018-10-30 上海新跃仪表厂 基于路标信息的航天器姿态指向误差辨识方法
CN105444778B (zh) * 2015-11-10 2018-10-09 北京空间飞行器总体设计部 一种基于成像几何反演的星敏感器在轨定姿误差获取方法
CN105528500B (zh) * 2016-01-19 2018-10-12 国家测绘地理信息局卫星测绘应用中心 一种分米级星载tdi ccd立体测绘相机成像仿真方法和系统
CN106289156B (zh) * 2016-09-28 2019-11-29 航天东方红卫星有限公司 一种卫星以任意姿态成像时获取摄影点太阳高度角的方法
KR101824191B1 (ko) * 2016-11-01 2018-01-31 한국항공우주연구원 위성영상 손실 인식 시스템, 방법 및 컴퓨터 판독 가능한 기록매체
US10533856B2 (en) * 2017-04-05 2020-01-14 Novatel Inc. Navigation system utilizing yaw rate constraint during inertial dead reckoning
CN107402004B (zh) * 2017-07-28 2021-03-09 歌尔光学科技有限公司 传感器的姿态信息获取方法及装置
KR101944631B1 (ko) * 2017-09-26 2019-01-31 주식회사 한화 사수의 조준 오차를 보정하는 무유도 로켓 조준 장치 및 그 방법
CN108413969B (zh) * 2018-01-31 2021-02-09 上海航天控制技术研究所 一种采用卫星影像辅助和无线通信网络的定位方法
CN110057382B (zh) * 2019-04-23 2021-07-09 西北工业大学 一种基于发射坐标系的捷联惯导数值更新方法
CN113340264B (zh) * 2020-03-02 2023-03-14 中航西飞民用飞机有限责任公司 一种飞机迎角传感器的安装角度调试方法和安装装置
CN111623775B (zh) * 2020-05-15 2022-10-04 天津时空经纬测控技术有限公司 运载体姿态测量系统、方法以及存储介质
CN114577208A (zh) * 2022-01-28 2022-06-03 北京空间飞行器总体设计部 一种基于旋转参考坐标系的导航系统误差统一建模方法

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US6125329A (en) * 1998-06-17 2000-09-26 Earth Satellite Corporation Method, system and programmed medium for massive geodetic block triangulation in satellite imaging
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US6233105B1 (en) * 1999-03-29 2001-05-15 Inventec Corporation Method of disk formatting

Also Published As

Publication number Publication date
US6336062B1 (en) 2002-01-01
JP3428539B2 (ja) 2003-07-22
EP1106505B1 (de) 2003-06-18
DE60003381T2 (de) 2004-05-19
JP2001165694A (ja) 2001-06-22
EP1106505A3 (de) 2002-08-14
EP1106505A2 (de) 2001-06-13

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