[HTML][HTML] A new thrust vector-controlled rocket based on JOA using MCDA
A thrust vector-controlled rocket model consists of army science board model responsible for
computing the angles of the gravity center with a directivity of trajectory positions (x, z). A …
computing the angles of the gravity center with a directivity of trajectory positions (x, z). A …
Conceptual design and analysis of a two-stage underwater glider for ultra-long voyage
An underwater glider (UG) designed for ultra-long voyage undoubtedly requires additional
battery energy, which is generally realized by increasing the volume. However, a larger …
battery energy, which is generally realized by increasing the volume. However, a larger …
A novel multidisciplinary hierarchical collaborative optimization of the high-speed pantograph considering the uncertainty of joint clearances
J Zhang, Y Tian, S Liu, W Zhang - Engineering Optimization, 2024 - Taylor & Francis
The pantograph–catenary system is a critical subsystem of the train power supply system.
However, the increasing train speed brings many challenges. In particular, the interaction …
However, the increasing train speed brings many challenges. In particular, the interaction …
Concurrent Trajectory Optimization and Aircraft Design for the Air Cargo Challenge Competition
NMB Matos, AC Marta - Aerospace, 2022 - mdpi.com
A coupled aerostructural aircraft design and trajectory optimization framework is developed
for the Air Cargo Challenge competition to maximize the expected score based on cargo …
for the Air Cargo Challenge competition to maximize the expected score based on cargo …
Integrated Orbital Design Method for Manned Lunar Exploration with Relaxed Temporal Constraints
An integrated orbital design method with relaxation of temporal constraints is presented,
focusing on improving the efficiency of complex-flight-mission planning for manned lunar …
focusing on improving the efficiency of complex-flight-mission planning for manned lunar …
Research on agile space emergency launching mission planning simulation and verification method
W Feng, L Xiuluo, W Jia, L Chao, L Ying… - Journal of Systems …, 2023 - ieeexplore.ieee.org
Space emergency launching is to send a satellite into space by using a rapid responsive
solid rocket in the bounded time to implement the emergency Earth observation mission …
solid rocket in the bounded time to implement the emergency Earth observation mission …
Coupled Vehicle and Trajectory Design Optimization for Boost-Glide Hypersonic Systems
JR Gottlieb, JM Mines, DC Garmendia… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
Multidisciplinary design optimization approaches have been successfully applied to many
flight vehicle design problems in academia and are now becoming more common in …
flight vehicle design problems in academia and are now becoming more common in …
Intelligent Systems in Space Transportation Industry
JAN Andrade - 2023 - search.proquest.com
Intelligent systems, and artificial intelligence specifically, have taken center stage in public
squares. New technological developments have led to the fomentation of high optimist …
squares. New technological developments have led to the fomentation of high optimist …
[PDF][PDF] Исследование динамики возмущенного движения многоразового упругого блока ракеты-носителя на участке посадки
ВВ Сметана, ИЕ Давыдов, АА Лазарев - engjournal.bmstu.ru
В ходе выполненного исследования определены параметры номинальной траектории,
а также проведена оценка динамики возмущенного движения возвращаемого упругого …
а также проведена оценка динамики возмущенного движения возвращаемого упругого …
[引用][C] 비정렬유동해석자를이용한비행체의공력특성분석
박상현, 이상봉, 권오준 - 한국항공우주학회학술발표회초록집, 2024 - dbpia.co.kr
일반적으로 비행체의 공력 설계에 있어 항력은 연료의 효율성 및 구조적 하중과 밀접한 연관이
있기 때문에 이를 정확히 해석하여 항력을 최대한 줄이는 것이, 매우 중요하다 항력은 …
있기 때문에 이를 정확히 해석하여 항력을 최대한 줄이는 것이, 매우 중요하다 항력은 …