147 | Task and attitude control scheduling of multiple agile satellites considering task-dependent transition time Kim, Junhong; Ahn, Jaemyung, AIAA Scitech 2020 Forum, American Institute of Aeronautics and Astronautics, 2020-01-10 |
148 | Task Scheduling of Agile Satellites with Transition Time and Stereoscopic Imaging Constraints Kim, Junhong; Ahn, Jaemyung; Choi, Han-Lim; Cho, Doo-Hyun, JOURNAL OF AEROSPACE INFORMATION SYSTEMS, v.17, no.6, pp.285 - 293, 2020-06 |
149 | Technology-aware complexity methodology for cost forecasting of space projects = 기술 발전을 고려한 복잡도 기반의 우주 프로젝트 비용 예측 방법론link Lee, Seung-Yup; Ahn, Jaemyung; et al, 한국과학기술원, 2022 |
150 | Three-Step Procedure for Landing of a Reusable Launch Vehicle Considering Flight Safety Yoon, Namkyung; Ahn, Jaemyung, 2017 Asia-Pacific International Symposium on Aerospace Technology, APISAT, 2017-10-17 |
151 | Time-Expanded Networks for Logistics of the Space Exploration Based on Mixed-Integer Linear Programming Lee, Juseong; Ahn, Jaemyung, 12th SIAM: East Asian Section Conference 2017, EASIAM, 2017-06-23 |
152 | Trajectory optimization and control algorithm of longitudinal perch landing assisted by thruster Tahk, Min-Jea; Han, Seungyeop; Lee, Byung Yoon; Ahn, Jaemyung, 2016 European Control Conference, ECC 2016, pp.2247 - 2252, Institute of Electrical and Electronics Engineers Inc., 2016-06 |
153 | Trajectory Optimization of a Launch Vehicle with Explicit Instantaneous Impact Point Constraints for Various Range Safety Requirements Yoon, Namkyung; Ahn, Jaemyung, JOURNAL OF AEROSPACE ENGINEERING, v.29, no.3, 2016-05 |
154 | Trajectory optimization of launch vehicle considering instantaneous impact point Yoon, Nam Kyung; Ahn, Jaemyung, 65th International Astronautical Congress 2014: Our World Needs Space, IAC 2014, pp.8099 - 8103, International Astronautical Federation, IAF, 2014-09 |
155 | Two-phase experimental design with adaptive subspacing for wind tunnel testing based aerodynamic modeling Lee, Dongoo; Jin, Hyeon; Shim, Ho-Joon; Ahn, Jaemyung; Choi, Han-Lim, JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, v.30, no.11, pp.5041 - 5050, 2016-11 |
156 | Two-phase framework for footprint prediction of space object reentry Kim, Siwoo; Jo, Byeong-Un; Choi, Eun-Jung; Cho, Sungki; Ahn, Jaemyung, ADVANCES IN SPACE RESEARCH, v.64, no.4, pp.824 - 835, 2019-08 |
157 | Two-phase framework for near-optimal multi-target Lambert rendezvous Bang, Jun; Ahn, Jaemyung, ADVANCES IN SPACE RESEARCH, v.61, no.5, pp.1273 - 1285, 2018-03 |
158 | UAV Mission Planning in Rechargeable Environment Using Vehicle Routing Problem with Profits(VRPP) Ko, Jaeyoul; Ahn, Jaemyung, 12th SIAM: East Asian Section Conference 2017, EASIAM, 2017-06-23 |
159 | Vehicle routing problem with vector profits with max-min criterion Lee, Dongoo; Ahn, Jaemyung, ENGINEERING OPTIMIZATION, v.51, no.2, pp.352 - 367, 2019-02 |
160 | Virtual Impact Point based Midcourse Guidance for Exo-Atmospheric Interception HWANG, JUNSUB; NA, HYUNGHO; Ahn, Jaemyung, 2023 Asia-Pacific International Symposium on Aerospace Technology, Asia-Pacific International Symposium on Aerospace Technology (APISAT), 2023-10-17 |
161 | Weapon–Target Assignment by Reinforcement Learning with Pointer Network Na, Hyungho; Ahn, Jaemyung; Moon, Il-Chul, JOURNAL OF AEROSPACE INFORMATION SYSTEMS, v.20, no.1, pp.53 - 59, 2023-01 |
162 | Yaw-Control Spoiler Design Using Design of Experiments Based Wind Tunnel Testing Jeong, Byeongmin; Lee, Dongoo; Shim, Ho-Joon; Ahn, Jaemyung; Choi, Han-Lim; Park, Seung-O; Oh, Se-Yoon, JOURNAL OF AIRCRAFT, v.52, no.2, pp.713 - 718, 2015-03 |
163 | 다수 정찰 위성의 최적 감시정찰 임무 스케줄링 = Optimal mission scheduling of multiple surveillance and reconnaissance satelliteslink 양유상; 안재명; et al, 한국과학기술원, 2023 |
164 | 모멘트 기반 질량추정을 이용한 고정익 무인항공기 초기 사이징 = Preliminary sizing of fixed-wing UAV using moment-based mass estimationlink 하현석; 안재명; et al, 한국과학기술원, 2022 |
165 | 복수 이해관계자 관점을 고려한 vehicle routing problem의 파레토 프론트 생성 = Pareto front generation for the vehicle routing problem with vector profitslink 고재열; 안재명; et al, 한국과학기술원, 2018 |
166 | 비행 안전을 고려한 우주발사체의 최적 단 설계 = Optimal staging design of a launch vehicle considering range safety operationslink 조병규; 안재명; et al, 한국과학기술원, 2021 |
167 | 실험계획법 적용 풍동시험 결과를 활용한 매립형 대기자료시스템 모델링 연구 = Flush air data system modeling using doe-based wind-tunnel testlink 이명섭; 안재명; et al, 한국과학기술원, 2023 |
168 | 우주 물체 충돌 위험 분석을 위한 이중 모드 프레임워크 Kim, Siwoo; Lee, Jinsung; Choi, Eun-Jung; Cho, Sungki; Ahn, Jaemyung, 우주기술과 응용, v.2, no.1, pp.13 - 29, 2022-02 |
169 | 재진입 우주 물체의 낙하 영역 예측을 위한 두 단계 프레임워크 = Two-phase framework for footprint prediction of space object reentrylink 김시우; 안재명; et al, 한국과학기술원, 2019 |
170 | 적응적 실험계획법의 풍동실험 적용방안 연구 = Application of adaptive design of experiments to wind tunnel testinglink 진현; Jin, Hyeon; et al, 한국과학기술원, 2016 |
171 | 지형을 고려한 행성 표면 샘플 채취 임무를 위한 호퍼와 로버 시스템의 트레이드 스터디 = Trade off study on planetary surface sample collection system considering terrain properties : Hopper versus Roverlink 이장원; 안재명; et al, 한국과학기술원, 2019 |
172 | 최적제어기법을 이용한 우주시스템의 동적 기술포트폴리오 최적화 = Dynamic technology portfolio selection of space system using optimal control theorylink 홍슬기; Hong, Seulki; et al, 한국과학기술원, 2016 |
173 | 컨벡스 최적화 기법을 이용한 재사용 발사체의 재진입 및 착륙 유도 = Re-entry and landing guidance of reusable launch vehicle using convex optimizationlink 황준섭; 안재명; et al, 한국과학기술원, 2021 |