自动驾驶仪

• This actuator is used in the longitudinal control system of fighter t improve longitudinal control and stability , and is a power actuating unit of autopilot
  用于歼击机纵向操纵系统，改善纵向操稳性能，也是自动驾驶仪的输出执行部件。
• Modern commercial aircraft operate on autopilot for much of the time , and they also land under automatic control at suitably equipped airports on a regular basis
  现代商用飞机大多时间是由自动驾驶仪操纵的，在装备完善的机场，这些飞机一向在自动控制指挥下着陆。
• And the traditional designed autopilot has poor robustness , so it should shift the autopilot ' s gain for the btt missile flying stably along the whole trajectory
  又由于用传统方法设计的自动驾驶仪鲁棒性不高，为控制导弹沿全弹道飞行，需逐段切换自动驾驶仪的增益。
• Steering by automatic pilot and by magnetic compass in stead of automatic pilot , measure the exactness of magnetic compass by qualified calibrator and provide compass adjustment card
  自动驾驶仪操舵和用磁罗经代替自动驾驶仪，通过合格的校准器来测定罗经的正确功能并提供罗经校正卡。
• By adopting the full state feedback approach and using the modeling aerodynamic interference as feedback nonlinearities , a new autopilot for uav close formation flight is designed
  采用全状态量反馈，同时将气动干扰作为非线性反馈，设计出一套适用于无人机近距离编队飞行的自动驾驶仪。
• Based on the relative position between the missile and the target at any given point in flight , the computer autopilot sends commands to the control surfaces to adjust the missile ' s course
  根据在给定时刻导弹和目标之间的相对位置，自动驾驶仪中的计算机发送指令到控制面，调整导弹的运动状态。
• Considering that the state variables can be measured easily and the autopilot can be designed expediently , the btt missile ' s control model in which all trajectory states can be measured is presented in this thesis
  并考虑到状态变量的可测量性和自动驾驶仪设计的方便性，建立了全弹道可测量的btt导弹控制数学模型。
• The main task of this dissertation is to digitize an autopilot system installed in a certain lateral airliner . the difficulty of this task is to design and manufacture a dissimilar redundancy fault - tolerant autopilot computer
  本论文的主要工作是对某支线客机自动驾驶仪进行数字化。该项工作的难点是非相似余度容错飞控计算机的研制。
• Firstly , the random mathematics model of the guidance system is set up , with the random factors such as the seeker , the guidance law , the automatic pilot , the dynamics , the relative kinematics taken into account
  首先进行反辐射无人机系统的随机建模，包括导引头、制导律、自动驾驶仪，机体动力学，相对运动学等，建模时必须考虑随机因素的影响。
• This group focus on the research of missile and launch vehicle , which contain the guidance law and the controller design . there are two researchers in this group now , including one m . d
  本研究群的宗旨乃进行拦截飞弹及运载火箭之研究，主要包含导引法则及自动驾驶仪控制器设计等项目，并利用各式各样的模拟(其中也包含空气动力学模型) ，验证其系统可行性。