launch direction 中文意思是什麼
launch direction
解釋
發射方向-
W, s, a, d keys control direction, the space bar to jump, aiming to control the mouse, the left mouse button launch, q key used flame - e button guns, p bond suspended
W s a d鍵控制方向，空格鍵跳躍，鼠標控制瞄準，鼠標左鍵發射， q鍵使用火焰噴射器， e鍵使用槍， p鍵暫停。 -
This scheme availes both to shorten launch distance and to shift shooting direction easily
採用此方案不僅大大縮短了瞄準距離，而且變換射向更為方便。 -
Loading screen will display a blank please wait patiently for the game : d ws a direction for the launch j bomb j k for the selection and start key
加載時畫面將顯示空白請耐心等待游戲方法： a s d w為方向j發射k爆彈j為選擇and開始鍵 -
Introduction : loading screen will display a blank please wait patiently for the game : d ws a direction for the launch j bomb j k for the selection and start key
攻略：加載時畫面將顯示空白請耐心等待游戲方法： a s d w為方向j發射k爆彈j為選擇and開始鍵 -
6. using simulation data of cz - 2f launch vehicle fault simulation system, the result of simulation based on cz - 2f launch vehicle pitch direction indicate that hm filtering fault detect can assure whether fault occurs, and this method achieves a better robustness and improves detect accuracy
以cz ? zf大型運載火箭作為研究對象，利用c2 ? 2f運載火箭故障模擬系統的模擬數據，使用h _濾波故障檢測方法對cz ? 2f運載火箭的俯仰通道進行了故障檢測模擬，通過對余量曲線的分析表明這種方法能較好的判斷故障是否發生，由此說明了利用h _濾波理論進行魯棒故障檢測的可行性。 -
Firstly, the task, structure, technology and function of the existing dispatch system were introduced, whose key technology is based on the tdm and time division switch like pstn. further, the developing direction of pstn is based on ip, the pocked switch system and network, and also the dispatch system of the manned space flight launch base will transmit multimedia information on ip
首先，介紹了現有調度系統的任務、結構、技術和功能，可以看出，其技術核心是時分多路復用和時分交換技術，現在公用交換電話網（ pstn ）正向基於ip的包交換系統和網路發展，載人航天發射場調度系統也將利用ip網路技術傳輸多媒體指揮信息。 -
The next key control about the direction z key to the net, x - key launch stars, h - bond renewed, w key changing clothes
上下左右鍵控制方向， z鍵為網子x鍵發射星星， h鍵換發型w鍵換衣服。 -
Launch process of missile, especially initial disturbance, is an important direction of launch dynamics. with the development of compute simulation and launch dynamics, much technology and method has been researched in the area of launch process
導彈發射過程，特別是導彈的初始擾動是發射系統研究的一個重要課題，隨著計算機模擬和發射動力學的發展，對導彈發射過程的研究也有許多不同的途徑和技術。 -
To assume responsibility, direction and support for the apqp launch team for both prototype and production requirements
要確保apqp發起團隊符合無論樣件還是大批生產要求的職責，方向及支持
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