公开(公告)号：KR20120019786A

公开(公告)日：2012-03-07

申请号：KR20100083227

申请日：2010-08-27

Applicant: KOREA AEROSPACE RES INST

Inventor： KIM HAE DONG

IPC: B64G1/10 ,  B64G1/24 ,  B64G1/40 ,  B64G3/00

CPC classification number: B64G1/10 ,  B64G1/242 ,  B64G3/00 ,  G06K7/00

Abstract: PURPOSE: A temporary satellite constellation design system and method for a reconnaissance and surveillance mission are provided to obtain the maximum observation effect from limited satellite resources by reconnoitering and surveilling a specific area using a small number of satellites. CONSTITUTION: A temporary satellite constellation design system comprises an input part(100), a design part(200), and an achievement calculation unit(300). The input part receives current orbit information on each satellite and target orbit information for rearranging satellites corresponding to temporary satellite constellation from outside and generates an input signal. The design part searches for a target orbit of each satellite based on the input signal of the input part and designs temporary satellite constellation. The achievement calculation unit calculates achievement according to the target orbits.

Abstract translation: 目的：提供一种用于侦察和监视任务的临时卫星星座设计系统和方法，通过使用少量卫星进行侦察和监视特定区域，从有限的卫星资源获得最大观测效果。 构成：临时卫星星座设计系统包括输入部分（100），设计部分（200）和成就计算单元（300）。 输入部分接收关于每个卫星的当前轨道信息和目标轨道信息，用于从外部重新排列对应于临时卫星星座的卫星，并产生输入信号。 设计部分基于输入部分的输入信号搜索每个卫星的目标轨道，并设计临时卫星星座。 成就计算单元根据目标轨迹计算成果。

公开(公告)号：EP3045393A4

公开(公告)日：2017-04-19

申请号：EP13875320

申请日：2013-12-13

Applicant: KOREA AEROSPACE RES INST

Inventor： LEE SANG CHERL ,  REW DONG YOUNG ,  SIM EUN SUP ,  CHOI GI HYUK ,  CHO DONG HYUN ,  KIM HAE DONG ,  KIM JEONG HOON ,  KIM IN KYU ,  MOON SANG MAN ,  HAN SANG HYUCK ,  MOON SUNG TAE ,  SUK JIN YOUNG ,  KIM JIN-WON ,  NO TAE SOO ,  GONG HYEON CHEOL ,  KIM MIN KI ,  KIM JONG CHUL

IPC: B64F1/00 ,  B64F1/22 ,  E04H6/44 ,  G08G5/00 ,  G08G5/02

CPC classification number: B64F1/222 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/141 ,  B64C2201/145 ,  B64C2201/208 ,  B64F1/007 ,  B64F1/362 ,  E04H6/44 ,  G05D1/042 ,  G08G5/0013 ,  G08G5/0069 ,  G08G5/025

Abstract: An apparatus and method of charging and housing of an unmanned vertical take-off and landing (VTOL) aircraft is disclosed. The apparatus includes an accommodator to accommodate an aircraft, a landing platform on which the aircraft lands, a housing portion to monitor state data by housing or charging the aircraft, and a sensor to assist in landing of the aircraft by allowing the aircraft to communicate with the apparatus. The apparatus enhances operational efficiency by reducing a travel time of the aircraft.