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Showing results 4 to 8 of 8

4
Guidance algorithm for ascending trajectory of supersonic engine vehicle = 초음속 엔진 비행체의 상승궤적 유도 알고리듬link

Kim, Keum-Seong; 김금성; et al, 한국과학기술원, 2012

5
Impact-time-control guidance laws for cooperative attack of multiple missiles = 다수 유도탄의 협력 공격을 위한 충돌시간제어 유도법칙link

Jeon, In-Soo; 전인수; et al, 한국과학기술원, 2007

6
L1 Penalized Sequential Convex Programming for Fast Trajectory Optimization: With Application to Optimal Missile Guidance

Roh, Heekun; Oh, Young-Jae; Tahk, Min-Jea; Kwon, Ki-Jeong; Kwon, Hyuck-Hoon, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.21, no.2, pp.493 - 503, 2020-06

7
Near Time-Optimal Feedback Instantaneous Impact Point (IIP) Guidance Law for Rocket

Jo, Byeongun; Ahn, Jaemyung, AEROSPACE SCIENCE AND TECHNOLOGY, v.76, pp.523 - 529, 2018-05

8
벡터필드 유도기법이 적용된 다수 무인기를 이용한 적 방공망 제압 임무의 실험적 검증

정우영; 김기덕; 이성헌; 방효충, 한국항공우주학회지, v.43, no.3, pp.282 - 287, 2015-03

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