UAV mathematics model is linearized by little disturbance method in equilibrium operating points, then linear controllers are design by applying eigenvalue configuration method to the linear models.
从无人机的数学模型出发，在特征点作小扰动线性化处理，采用特征值配置法对线性化对象设计线性控制器。
Firstly, the paper introduce the process of design the UAV AFCS, which use the test of model fly to confirm the control principle parameter.
本文首先介绍了无人机飞控系统的设计过程，采用模型飞行试验进行控制律参数设置与确定。
Firstly, the features of UAV task assignment are analyzed in depth, and then the extended mixed integer linear programming (MILP) model for task assignment is established.
本文首先深入分析多无人机任务分配问题的特点，建立了扩展的混合整数线性规划(MILP)任务分配模型。
This paper researches the method of modeling and principle of establishing model of unmanned aerial vehicle(UAV) during gliding with rudder lock-in-place.
本文研究无人机方向舵卡死时下滑模型建立的方法与处理原则。
With the problem of path planning of reconnaissance UAV, its influential factors and model are analyzed.
文章针对侦察无人机航路规划这一问题，分析了影响航路规划的因素，构建了航路规划的模型。
The model of a UAV formation is decomposed into the decoupled part and the interconnected part.
将无人机编队模型分解成解耦部分和关联部分。
Then a cooperative planning model was established, which could plan a feasible path for each UAV, which meeted both the requirements of time-coordination and the minimum cost.
然后建立协同模型，为各无人机规划出既能满足时间协同要求，又能满足整体代价最优的可行航迹。
The model built in this paper has great significance to performance simulation of the UAV communication channel when no measurement data are available.
对于当前没有较完备的无人机通信系统实测数据时，进行无人机通信信道的统计模型建立和仿真等方面的研究具有重要意义。
A model is built based on support vector machine (SVM) for predicting the military unmanned air vehicle (UAV) development cost prediction.
应用支持向量机建立了军用无人机研制费用预测模型，并采用该模型对某型军用无人机研制费用进行了预测。
Bases on the aircraft structure fatigue life theory, consider the characteristics of small UAV, the model of fatigue life prediction for small UVA structure is established.
在飞机结构寿命理论的基础上，结合小型无人机机体结构特点，建立了小型无人机机体寿命分析方法。
Due to the limit of traditional UAV navigation control, this paper puts forward a kind of navigation control system that is based on the strategy of multi-model variable structure intelligent control.
针对传统无人机导航控制的局限性，提出基于多模变结构智能控制策略的导航控制系统。
Due to the limit of traditional UAV navigation control, this paper puts forward a kind of navigation control system that is based on the strategy of multi-model variable structure intelligent control.
针对传统无人机导航控制的局限性，提出基于多模变结构智能控制策略的导航控制系统。
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