控制定律 的英文怎麼說
中文拼音 [kòngzhìdìnglǜ]
控制定律
英文
control law- 控 : 動詞1 (告發;控告) accuse; charge 2 (控制) control; dominate 3 (使容器口兒朝下 讓裏面的液體慢...
- 制 : Ⅰ動詞1 (製造) make; manufacture 2 (擬訂; 規定) draw up; establish 3 (用強力約束; 限定; 管束...
- 定 : Ⅰ形容詞1 (平靜; 穩定) calm; stable 2 (已經確定的; 不改變的) fixed; settled; established Ⅱ動詞...
- 律 : Ⅰ名1 (法律; 規則) law; rule; statute; regulation 2 (律詩的簡稱) short for lüshi 3 (姓氏) a ...
- 控制 : control; dominate; regulate; govern; manage; check; cybernate; manipulate; encraty; rule; rein; c...
-
According to the direction and damping characteristic of the torque produced by the magnetorquers, the three axis attitude control schemes of gravity gradient satellite and other satellite with damper is presented. the control coefficients are determined by the dynamic characteristics of geomagnetic intensity, so the attitude control precision is improved
根據磁力矩在地磁場中的定向阻尼特性,提出了磁控重力梯度衛星和攜帶阻尼器的非重力梯度姿態控制規律,根據地磁場強度變化規律選擇控制系數,提高衛星的姿態控制精度。In ship steering controller design, the nonlinear ship model should be written in siso strict feedback form. we start the recursive design with the system first state variable and continue with the second one. by introducing a change of coordinates, we choose lyapunov functions to stabilize the system and obtain the control law
在船舶航向控制方面,考慮船舶的穩態回轉非線性,應用backstepping方法設計:首先把系統化成單入單出的嚴格反饋控制形式(呈下三角結構) ,假設系統后一個狀態變量是前一個狀態變量的虛擬控制,通過適當的變量代換,在每一步構造李亞普諾夫函數,使前一子系統在虛擬控制下漸近穩定,逐步遞推出控制器控制規律,使整個系統在平衡點滿足一致漸近穩定性。And the outcomes is are better effective. combining fuzzy logic control with pid control algorithm, this paper ana1yses the rule of fuzzy adaptive pid control, furthermore optimizes the rules of fuzzy longic control based on classification and
將模糊控制與pid演算法相結合,提出了模糊自整定pid控制的控制規律,並應用模糊盒樹法對模糊控制規則進行優化,從而得到一種控制規則簡單,控制性能良好的控制方法。In this paper, the design of electric forklift driving controller is demonstrated. otherwise, can is added into this controller, so as to build up can networks with other modules equipped with can controllers. this paper is composed of 7 chapters : in the first chapter, the background of the paper is introduced ; in the second chapter, the structure of electric forklift is demonstrated ; in the third chapter, first the math model of series motor is found, then the motor is controlled as improved p1d control rule ; in the fourth chapter, the principle and realization method of forward and reverse rotation and back - feed brake are explained ; in the fifth chapter, the principle of can and design of application layer in can are illuminated ; in the sixth chapter, the principle of e2prom is clarified ; in the last chapter, summary of the whole paper is given, and prospect in this field is made
全文共分七章:第一章緒論,介紹了論文背景;第二章,系統綜述,介紹了電動叉車的整車結構;第三章,串勵電機的建模、改進的pid演算法及其軟硬體實現,首先根據串勵電機的機電特性推導出數學模型,然後在此基礎上結合pid控制規律對電機進行控制;第四章,串勵電機的正反轉及回饋制動,介紹了實現電機正反轉及回饋制動的原理及方法;第五章, can網路實現模塊間通訊,介紹了can總線原理及can總線應用層設計;第六章,用串列e ~ 2prom實現參數設定,介紹了串列e ~ 2prom的原理;結束語,對本論文進行了總結,並對該領域的發展進行了展望。In this thesis, based on mathematic model and real condition, analysis and compare of different control methods are carried out at first. then a propriety control law and optimized parameters are choosen and used into multi - body model in simpack. finally, kinds of dynamic character curves after measurement and calculation are given
論文首先在數學建模的基礎上,根據實際情況,詳細分析對比了直接狀態反饋控制、 pid控制和狀態觀測器控制等常用的磁浮列車懸浮控制方法,然後將合適的控制規律及優化的控制參數用於simpack中的多體模型,通過計算,給出懸浮穩定性、運行平穩性以及列車曲線通過等動力學特性曲線。Based on the theory of associated and decentralized control, this paper introduces the modeling method of ac / dc power system and control law deriving, which can be realized dispersedly and guarantee the stability of the system with optimal performance
摘要介紹了交直流電力系統關聯測量分散勵磁控制的建模方法和控制規律的求取,所得控制規律既可以分散實現,又能保證全局穩定且性能最優。This paper studies on the attitude ontrol system of three - axis stabilized satellite systematically, and makes deep study on the design of attitude control system. the main work of this paper is as follows : first, found whole mathematical model about attitude control system of satellite. it contains kinematics model, dynamic model, actuator model and torque model. analyse the conmmen characteristic of actuator of satellite ’ s attitude control system
本文較為系統地研究了三軸穩定衛星的姿態控制系統,並在姿態控制規律的設計方面進行了較為深入的研究。論文主要工作如下:首先,建立了完整的衛星姿態控制系統的數學模型。其中包括星體運動學模型、星體動力學模型、執行機構模型及環境干擾力矩模型。This research can determine the assist control strategy, the basic parameters and steering perform standard of electric power steering
對電動助力轉向助力控制規律、基本設計參數以及相關試驗標準的確定有指導意義。Second, the damp loop and the center of mass stabilization loop are simulated by traditional pid control theory, the problem lied in the application of the pid control theory is analyzed
第二,利用傳統pid控制規律對導彈的阻尼迴路和質心穩定迴路進行了設計模擬,並對pid控制規律在導彈控制迴路中的應用所存在的問題作了分析。The fourth part analyzed the intermediate dc voltage and its control principle and the technical parameter of the main parts in the ac transmission system. several key technical problems such as parallel working of the ac motors, the wheel diameter difference under the bogie - control mode, the ac motor - inverter matching principle are studied in detail. the principles to determine the electrical parameters are also discussed
論文第4章重點研究了變流器的中間直流電壓的確定及其控制規律,確定了交流電傳動系統主要部件的技術參數;研究了架控方式工作下電動機並聯工作、輪徑差、電機?變流器匹配原則等關鍵的技術問題;詳細分析了交流傳動系統在牽引工況和電阻制動工況下各參數的工作過程和控制原則。In this paper, to resolve the coupling phenomena between temperature and humidity in wood drying system, a bp neural network based pid controller is proposed and applied to wood drying system. the architecture and learning algorithm of the proposed controller is more simpler and the physical meanings of the input layer ' s neurons and output layer ' s neurons are explicit. based on predefined control rules and self - learning, the bp network changs the scaling integral and differential parameters, therefore is able to control the variants using classical pid control algorithms and at the same time, decoupling control is implemented as well during the control procedure
本文針對木材幹燥過程中溫、濕度耦合的現象,提出一種將新的基於bp神經網路的pid控制器應用於木材幹燥控制系統的方案,其結構和學習演算法相對簡單,輸入層和輸出層神經元物理意義明確;它根據設定的某一控制規律,通過網路的自學習,調整pid控制器的比例、積分和微分參數,從而利用經典的pid控制演算法得到相應各變量的控制量參與控制,並在該過程中實現解耦控制,而不用給定樣本信號進行在線的學習。According to the direction and damping characteristic of magnetic torque and the theory of linearity, the scheme of satellite attitude control just using magnetic torque is presented
根據地磁力矩定向阻尼特性和線性疊加理論,提出僅用磁力矩器實現對地指向衛星三軸姿態穩定的控制規律。Aiming at the advantages and disadvantages of existing lighting control systems, it is very essential to develop a residence lighting smart control system for intelligent architecture ' s development and people ' s life quality improvement according to the control law determined by people ' s behavior pattern and residence luminous environment
針對現有智能照明控制系統的優、缺點,根據人們的行為模式和住宅的光環境決定照明的控制規律,研製住宅智能照明控制系統對智能建築的發展、提高人們的生活質量具有重要的意義。At last, this paper realizes the sonar array attitude stabilization system based on the simulation circuitry and introduces the method of how to make control system with pc / 104. the attitude stabilization system is debugged successfully.
最後,對上述聲納基陣姿態穩定系統進行了基於模擬電路的硬體實現,應用pc 104實現控制規律,並對整個系統進行調試。Third, the center of mass stabilization loop is designed by the proportion control law in variable structure control, the design method of the proportion control law is deducted elaborately. the result is the character points is unified on parameter. the two simulation results of the different methods are compared in this paper
第三,利用變結構控制中的比例控制規律對導彈的質心穩定迴路進行了設計,詳細推導了比例控制規律的設計方法,實現了各個特徵點設計參數上統一,並對前面兩種設計方法的模擬結果進行了比較,最後還討論了兩種設計方法對干擾的抑制作用。On the basis of that, linear state feedback control law is designed to ensure the stability and security of power system
在此基礎上,設計線性狀態反饋控制規律,使得電力系統的運動狀態保持穩定。The cost function of the optimal control problem is a weighted sum of the squared horizontal and vertical components of the helicopter velocity at touchdown. the control ( horizontal and vertical components of the thrust coefficient ) required to minimize the cost function is obtained using nonlinear optimal control theory
其次,定義最優控制問題的性能指標為直升機著陸時的水平和垂直速度的加權平方和為最小,並採用一階梯度演算法得到使性能指標最小的控制規律。Green " s theorem is employed to find the quantity relationship among the constraints of heating rate, dynamic pressure and lift in reentry flight. the paper deduced the approximate solution of the optimal aeroassisted coplanar trajectories under the three typical constraints. the performance index to be minimized are either heat input, the total dynamic pressure, time during the atmospheric flight, the time integral of the square of the path inclination ; or maximize the time of flight during the atmospheric portion of the trajetory. an important conclusion is firstly obtained : under the three constraints above, the optimal aeroassisted coplanar transfers with the first forth kinds payoffs have the same optimal control laws
採用格林函數法,給出了同一平面氣動力輔助變軌飛行的3種過程約束(氣動加熱率、動壓、升力約束)條件之間關系的近似定量描述形成的飛行包絡線.由此求解了航天器同時受3種約束條件時,各種性能指標下的同一平面氣動力輔助變軌軌跡的近似解及相應的最優控制規律.文中對近似解與控制規律的內部結構作了細致的分析,得到了一些有益的結論Through the analysis of the attitude dynamic equation, the potential energy function is derived. the relationships of attitude varieties are derived from energy function and angle momentum equation and thus the attitude control laws of bias momentum satellite are put forward
通過對衛星姿態動力學方程分析,得出衛星的勢函數,結合衛星的勢函數和角動量方程導出各姿態之間變化關系,提出利用地磁場實現偏置動量輪衛星姿態穩定的控制規律。The system based on pid control theory has characteristics of fast response speed and higher peak overshoot, and it also has a good performance of tracking, but it is lack of ability of disturbance rejection. because smvs control method is insensitive to the variations of the model parameters, nonlinear and exterior noises, the attitude stabilization system designed based on smvs has fast response speed, higher ability of disturbance rejection and has no peak overshoot, namely, the system is robust
模擬結果表明,基於pid控制規律設計的系統具有響應速度快但超調大的特點,系統的跟蹤性能較好,但抗干擾能力較差;滑模變結構控制方法因為其對模型參數的變化、非線性和外擾噪聲的不敏感性,設計的聲納基陣姿態穩定系統無超調,響應速度快而且抗干擾能力強,具有很好的魯棒性。分享友人