导航定位学报
導航定位學報
도항정위학보
Journal of Navigation and Positioning
2015年
3期
100-104
,共5页
遥感卫星%临界回归椭圆轨道%临界轨道%回归轨道%区域覆盖
遙感衛星%臨界迴歸橢圓軌道%臨界軌道%迴歸軌道%區域覆蓋
요감위성%림계회귀타원궤도%림계궤도%회귀궤도%구역복개
remote sensing satellite%critical regressive elliptical orbit%critical orbit%regressive orbit%regional coverage
在航天遥感任务分析与设计过程中,特殊类型轨道(太阳同步轨道、回归轨道等)是卫星轨道设计的重要选择。当前遥感卫星轨道设计研究主要集中于太阳同步、回归的圆轨道设计方面,此类轨道具有全球覆盖、固定重访周期等独特优势,但是,面向热点区域侦察与监控等区域覆盖任务时,太阳同步轨道难以保证对特定目标的高分辨率成像和快速重访。本文针对区域覆盖任务需求,在介绍临界轨道、回归轨道特点基础上,提出了一种椭圆临界回归轨道遥感卫星轨道设计方法,通过引入回归特性定量描述参数,分析了回归系数的影响因素,提出了具有拱线静止特性椭圆轨道的设计流程,并根据区域覆盖要求给出了轨道设计算例,最后椭圆临界回归轨道的特性、适用任务类型进行了分析,算例表明该种轨道可对局部目标实施高分辨率成像,缩短轨道的回归周期,还保证了对同一纬度目标成像时分辨率一致。
在航天遙感任務分析與設計過程中,特殊類型軌道(太暘同步軌道、迴歸軌道等)是衛星軌道設計的重要選擇。噹前遙感衛星軌道設計研究主要集中于太暘同步、迴歸的圓軌道設計方麵,此類軌道具有全毬覆蓋、固定重訪週期等獨特優勢,但是,麵嚮熱點區域偵察與鑑控等區域覆蓋任務時,太暘同步軌道難以保證對特定目標的高分辨率成像和快速重訪。本文針對區域覆蓋任務需求,在介紹臨界軌道、迴歸軌道特點基礎上,提齣瞭一種橢圓臨界迴歸軌道遙感衛星軌道設計方法,通過引入迴歸特性定量描述參數,分析瞭迴歸繫數的影響因素,提齣瞭具有拱線靜止特性橢圓軌道的設計流程,併根據區域覆蓋要求給齣瞭軌道設計算例,最後橢圓臨界迴歸軌道的特性、適用任務類型進行瞭分析,算例錶明該種軌道可對跼部目標實施高分辨率成像,縮短軌道的迴歸週期,還保證瞭對同一緯度目標成像時分辨率一緻。
재항천요감임무분석여설계과정중,특수류형궤도(태양동보궤도、회귀궤도등)시위성궤도설계적중요선택。당전요감위성궤도설계연구주요집중우태양동보、회귀적원궤도설계방면,차류궤도구유전구복개、고정중방주기등독특우세,단시,면향열점구역정찰여감공등구역복개임무시,태양동보궤도난이보증대특정목표적고분변솔성상화쾌속중방。본문침대구역복개임무수구,재개소림계궤도、회귀궤도특점기출상,제출료일충타원림계회귀궤도요감위성궤도설계방법,통과인입회귀특성정량묘술삼수,분석료회귀계수적영향인소,제출료구유공선정지특성타원궤도적설계류정,병근거구역복개요구급출료궤도설계산례,최후타원림계회귀궤도적특성、괄용임무류형진행료분석,산례표명해충궤도가대국부목표실시고분변솔성상,축단궤도적회귀주기,환보증료대동일위도목표성상시분변솔일치。
Special types of orbit,such as sun-synchronous orbit,regressive orbit,are the first choices for low-orbit opti-cal remote sensing satellite.Currently design of remote sensing satellites orbit focuses on the sun-synchronous regressive circu-lar orbit,which has a unique advantage of global coverage,fixed revisit period.However,when orient to reconnaissance and surveillance mission for specific area,sun-synchronous is difficult to guarantee high-resolution imaging and rapid re-vis-it.Aiming at regional coverage mission requirements,a critical regressive elliptical orbit (CRE orbit)design method is pro-posed in this paper.Firstly,the characteristics and selection principles are briefly introduced;then by introducing a regression coefficient Q and analyzing the quantitative relationship between Q and orbit elements,design flow of CRE orbit is introduced;Thirdly,a calculation example of CRE orbit design is put forward based on proposed method;Finally,the characteristics of CRE orbit and its application task is discussed,the example shows that this kind of orbit can ensure the local targets high-reso-lution imaging,shorten the revisit period with a short revisit period,also maintain the uniformity of imaging resolution for the targets located in the same latitude.