DSpace at KOASAS
Browsing DSpace

Browse by Subject Guidance

A to Z

All 0-9

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

or enter first few letters:

Showing results 1 to 8 of 8

1
(A) method for reusable modeling and simulation software in aerospace engineering = 항공우주공학에서 재사용 가능한 M&S 소프트웨어를 위한 방법link

Ahn, Jong-Sun; 안종선; et al, 한국과학기술원, 2011

2
(A) method for reusable modeling and simulation software in aerospace engineering = 항공우주공학에서 재사용 가능한 M&S 소프트웨어를 위한 방법link

Ahn, Jong-Sun; 안종선; et al, 한국과학기술원, 2011

3
Discipline vs guidance: comparison of visual engagement approaches in immersive virtual environments

Lee, Hyeopwoo; Jung, Jinki; Lee, Heung-Kyu; Yang, Hyun Seung, MULTIMEDIA TOOLS AND APPLICATIONS, v.80, no.20, pp.31239 - 31261, 2021-08

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

Discover

rss_1.0 rss_2.0 atom_1.0