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Exploration of the Development Road for Chinese Liquid Rocket Engine in 21st Century
Wang Heng
Strategic Study of CAE 1999, Volume 1, Issue 2, Pages 1-5
Liquid rocket engine is an important member of the space propulsion family and the only propellingMeanwhile, we should begin preliminary researches on rocket spaceplane and aerospike nozzle adopted by
Keywords: propulsion having top priority liquid rocket engine heavy lift launch vehicle rocket spaceplane
XB High Accuracy Rocket Sled Test Track
Yang Xingbang
Strategic Study of CAE 2000, Volume 2, Issue 10, Pages 98-104
Rocket sled test track is a large ground dynamic simulating test facility.China has successfully built the world ´s only track —XB high accuracy rocket sled test track
Keywords: rocket sled test track ground dynamic simulating test
Astronauts Hitch First Ride Aboard Private Rocket to Space Station
Chris Palmer
Engineering 2020, Volume 6, Issue 11, Pages 1207-1209 doi: 10.1016/j.eng.2020.08.007
Lateral Vibration Analyses of Flying Vehicle under Thrust and Drag
Song Jian
Strategic Study of CAE 2000, Volume 2, Issue 10, Pages 63-72
In this paper, the influence of thrust and air drag on rocket lateral vibration is studied, and theThe equations of transverse movement when nozzle connected rigidly with rocket and related boundary conditions
Keywords: aircraft rocket lateral vibration thrust and drag vibration mode and frequency
Optimal Robust Control of AC Position Servo System for Multiple Rockets
Chai Huawei,Ma Dawei,Li Zhigang,Le Guigao,Wang Feng
Strategic Study of CAE 2007, Volume 9, Issue 10, Pages 83-87
In order to realize high speed and high precision position control in an AC servo system, in view of such kinds of uncertainties as moment of inertia and load moment changing widely, and strong impact moment, an optimal robust control tactics is put forward. Experimental results show that this control tactics has strong robustness, and has fairly good dynamic performances and steady-state precision.
Keywords: rocket mortar AC position servo system robust control optimal control
A composite optimization method for separation parameters of large-eccentricity pico-satellites None
Lai TENG, Zhong-he JIN
Frontiers of Information Technology & Electronic Engineering 2018, Volume 19, Issue 5, Pages 685-698 doi: 10.1631/FITEE.1700416
Keywords: Pico-satellite Satellite–rocket separation mechanism Separation parameters Parameter optimization
The Present Situation and Prospect of China's Space-entering Capacity
Long Lehao,Wang Xiaojun,Guo Linli
Strategic Study of CAE 2006, Volume 8, Issue 11, Pages 25-28
Keywords: space activities “Long-March” rocket family manned lunar landing reusable launching vehicles
Title Author Date Type Operation
Exploration of the Development Road for Chinese Liquid Rocket Engine in 21st Century
Wang Heng
Journal Article
Optimal Robust Control of AC Position Servo System for Multiple Rockets
Chai Huawei,Ma Dawei,Li Zhigang,Le Guigao,Wang Feng
Journal Article
A composite optimization method for separation parameters of large-eccentricity pico-satellites
Lai TENG, Zhong-he JIN
Journal Article