A brief review of flight mechanics research activities at home and abroad has been carried out. Some proposals to bring flight mechanics into full play in the development of future unmanned flying vehicle, guided missile and other munitions have been made.

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And the basic construction and run flow process of the software system are studied. Some applications programmes in flight mechanics are designed.

对软件系统基本结构和运行流程进行了分析研究，完成导弹设计不同阶段有关飞行力学问题研究的应用软件设计开发。

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On the basis of summarizing the imagery tracking algorithms, this thesis put forward a novel fundamental idea and steps of automatic target tracking algorithm that is specially fit for flight mechanics.

在综述了各种成像跟踪算法的基础上，给出了一种新的适于飞行力学自动目标跟踪算法的基本思想和方法步骤。

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The important roles of Auto-Flight Mechanics and Computational Flight Mechanics in the development of future flying vehicle are specially analyzed;

特别讨论了自控飞行力学和计算飞行力学在未来飞行器发展中的重要意义；

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Modal aggregation and its application in flight mechanics

模态集结法及其在飞行力学中的应用

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Equations of flight mechanics considering atmospheric turbulence

考虑大气扰动的飞行力学方程

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Design of Flight Mechanics Software System of Tactical Missiles

战术弹飞行力学软件系统设计

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The important roles of computational flight mechanics are further analyzed.

飞行控制计算机是飞行控制系统的核心。

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The evolutionary process of flight mechanics is discussed from the viewpoint of" Needs-Pulling and Speciality-Pushing";

从需求牵引和专业推动的观点出发，讨论了飞行力学的发展历程；

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Finally, Some proposals for Flight Mechanics of guided missile towards the 21st century have been made.

最后，对迈向21世纪的我国导弹飞行力学学科的建设和研究工作提出了一些看法和建议。

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Role of Experimental Design in Computational Flight Mechanics

计算飞行力学与试验设计

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The applications of the uniform experimental design and Monte Carlo testing method to computational flight mechanics are emphasized.

重点介绍了均匀试验设计法和统计试验法在计算飞行力学中的应用。

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Development of computational flight mechanics

计算飞行力学的产生和发展

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So, IAAP is an interdisciplinary-science, which bridges the flight mechanics, aerodynamics, elasticity and cybernetics.

它是处于空气动力学、飞行力学、弹性力学和现代控制论之间的应用性研究课题。

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Flight mechanics in the information age

信息时代的飞行力学

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In this paper, the problem in flight mechanics and aerodynamics for rolling resonance of the re-entry body are discussed;

本文综述了再入体滚转共振的飞行力学和气动力学问题；

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The important roles of experimental design in computational flight mechanics have been discussed;

讨论了试验设计在计算飞行力学中的重要意义；

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Making an example of a high-gain CAS ( Control Augmentation System), this paper deals with the design of main parameters of a CAS and the rela-tion between these parameters and an aircraft flight character, from the angle of flight mechanics.

本文从飞行力学的角度出发，着重以高增益控制增稳系统为主来讨论控制增稳系统的主要参数的设计及其同飞行品质的关系问题。

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A flight mechanics and stable control loop model of interception missile with the blended control by aerodynamic force and moment-gas-thrust-vector

空气动力和直接侧向力复合控制的拦截弹飞行力学及稳定回路模型

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Some Problems of Flight Mechanics in the Improvements of Guided Missile

导弹改进、改型中的飞行力学问题

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Flight Mechanics Towards the 21st Century

迈向21世纪的飞行力学

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