proportional guidance 中文意思是什麼

proportional guidance 解釋
比例導引法
  • proportional : adj （成）比例的；相稱的，平衡的，調和的 （to）。 a proportional number 比例數。 a proportional e...
  • guidance : n. 1. 向導，指引，指導。2. 導航；制導。3. 【機械工程】導槽，導板，導管。
  1. Simulation studies show that the proposed law in this paper has better guidance accuracy and better dynamic property during pursuit - control processing and it is superior to proportional navigation

    模擬結果表明，給出的導引律在攻擊機動目標時制導精度高、脫靶量小，導引控制過程具有良好的動態性，性能明顯優于傳統的比例導引律。
  2. Study of target acquisition probability for laser - guided bombs with proportional navigation guidance law

    激光比例制導航彈對目標的捕獲概率分析
  3. Effective guidance is one of the most important tasks to the performance of air - to - air missile. based on the proportional navigation, fuzzy logic and genetic algorithm are combined to develop an evolutionary fuzzy guidance 1 aw with s elf - adapt region for the air - to - air missile guidance

    並在傳統的模糊邏輯控制基礎上引入了一個非線性變論域函數，從而實現了模糊變量論域的動態改變，然後使用遺傳演算法對導引規則進行了尋優。
  4. Like proportional navigation guidance ( png ), the new guidance law, which utilizes line - of - sight ( los ) measurement only, is simple in implementing

    在執行上，變結構制導律僅使用了視線轉率測量值，因而和比例導引同樣簡單。
  5. In part iv, a kinematics model for 3d guidance problems is derived. then pure proportional navigation, approaching method, and fuzzy logic algorithm are combined to develop a three - dimension fuzzy guidance law. finally, this thesis expounds the modeling technology of 3d objects in computer animation simulation and the method of using opengl engine in visual c + + environment

    第四部分建立了三維空間中導彈追擊目標的運動學關系模型，分析了兩種古典導引律（平行接近法和比例導引法）的優缺點，在此基礎上提出了一種三維組合導引律，然後用模糊邏輯對其進行了優化，獲得了一種性能更為優越的三維模糊導引律，最後通過模擬證明該方法的優越性。
  6. To overcome the shortages of the traditional proportional guidance in attacking maneuvering targets, the paper firstly established the relative motion models for the anti - ship missile and the target in three dimensions, then based on the optimal guidance law for aiming at non maneuvering targets and the sliding - mode control theory, the optimal sliding - mode guidance law in three dimensions, which was more easily - accomplished in engineering, was derived by making the pitch plane and yaw plane superposition

    摘要針對傳統比例導引法攻擊機動目標的不足，建立了三維空間中反艦導彈和目標的相對運動模型，在研究反艦導彈攻擊非機動目標的最優制導律基礎上，利用俯仰和偏航兩個平面相疊加的方法，結合滑模控制理論設計了工程上易於實現的三維模型下的反艦導彈最優滑模製導律。
  7. Two parameters of this guidance law determine the relative importance of pursuit guidance and proportional guidance laws

    通過調整兩種導引法的系數決定其在導引法中的權重。
  8. Based on the pursuit guidance law and the proportional guidance law, a new guidance law is proposed for space intercept

    摘要基於追蹤導引律和比例導引律，提出了一種新的空間攔截末制導律。
  9. Using the sampled controlling parameters of the aircraft under pure proportional navigation ( ppn ), the thesis designs the corresponding discrete input signal of the guidance controller under the inside demand of the pursuing control, and trains a module of rbf off - line. then, the module is inserted into the control system of the aircraft and acted as its control input in order that the optimal function of the aircraft under ppn can be realized

    在分析比例導引律導引載機追蹤/截獲目標的狀態軌跡的基礎上，闡述徑向基神經網路的非線性功能特點，根據載機追捕目標的內在要求，設計並訓練徑向神經網路模塊，嵌入載機導引器的控制迴路，實現優化載機導引控制。
  10. 5. aiming at the specific mission that intercept the warhead of tactical ballistic missile, the new issue for designing the guidance law is analyzed, and a new guidance method that fit for the mid - course is presented, based on the idea of predicting the intercept point. to design a feasible terminal guidance law, the shortcoming existing in the proportional navigation when intercepting the warhead is firstly

    針對攔截戰術彈道導彈這一特殊任務，分析了導引律設計面臨的新問題，提出了以預測攔截命中點為思想的中制導段導引方法，研究了末制導段比例導引律彈道形狀和過載分佈特點，在此基礎上為了改善比例導引律的缺陷，引入了目摘『要標機動加速度和導彈軸向加速度等信息、 ，又寸比例導引律進行了修正，井對導引律中各參數進行了優化。
  11. Design and identification on parameters of proportional navigation guidance law with gravity over compensation

    帶過重力補償的比例導引制導律參數設計與辨識
  12. Simulations show that the variable structure guidance law yields much better performance compared to proportional navigation

    模擬結果表明，所提出的制導律與比例導引相比有較大的性能改善。
  13. The designed robust guidance laws are used to the simulation of air - air missile ' s attack process. the designed robust guidance laws are more valid than the proportional navigation guidance law

    與傳統的比例制導律相比，所設計的h 』魯棒制導律效果更好，魯棒性更強。
  14. Two spacecraft ’ s rendezvous technology in coplanar near - earth orbit with maneuvering target, based on the sight coordinate system is presented in this paper. differential games guidance law ( dggl ) and proportional navigation ( pn ) are studied

    本論文研究了近地共面軌道兩空間飛行器在目標機動下的在軌交會技術，分別對微分對策制導律和比例導引制導律兩種制導方法進行了研究。
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