In the second part : the active control system is detailedly designed 第二部分是設(shè)計電控主動減振系統(tǒng)。
Design and realization of active control system of vibration based on fpga 的振動主動控制系統(tǒng)的設(shè)計與實(shí)現(xiàn)
Time-delay compensation for semi-active control system of structural vibration 結(jié)構(gòu)振動半主動控制系統(tǒng)的時滯與補(bǔ)償
Discussion on the maximum allowable time-delay and stability of the structure-modal active control system 模態(tài)主動控制系統(tǒng)的最大允許時滯及穩(wěn)定性探討
Simulations are formed for the passive control system and active control system with different controller (4)比較了被動控制系統(tǒng)與主動控制系統(tǒng)的性能。
The ability of the active control system is increased because the response of structure is predicted by the ann 并通過神經(jīng)網(wǎng)絡(luò)系統(tǒng)對結(jié)構(gòu)響應(yīng)進(jìn)行一步預(yù)測,從而進(jìn)一步提高控制系統(tǒng)的能力。
The main work of this thesis : 1 . the mathematical model describing the landing gear active control system is established 本文的主要工作有以下幾個方面:(1)建立了飛機(jī)起落架緩沖器主動控制系統(tǒng)的數(shù)學(xué)模型。
In the third part : according to the active control system, experiment is carried out and the result of the experiment is detailedly analyzed 第三部分根據(jù)設(shè)計的電控減振系統(tǒng)對柴油機(jī)進(jìn)行了振動主動控制的實(shí)驗(yàn)。
The motion equation with time delay is presented . the time delay effects on the performance of active control system for platforms are investigated 建立了包含時間滯后的海洋平臺-主動控制裝置的振動控制方程,分析了時間滯后對主動控制所產(chǎn)生的不利影響。
When it comes to the aeroservoealstic analysis and design, the first problem is to construct a reduced order model, convenient to the design of active control system 研究氣動伺服彈性分析與設(shè)計,首要的問題是建立一個便于進(jìn)行主動控制系統(tǒng)設(shè)計的低階模型。