主从编队反舰导弹末制导段一体化位姿控制  

Integrated Control of Position and Attitude for Terminal Guidance of Leader-Follower Anti-Ship Missiles

作　　者：吴云洁[1,2,3] 张聪[1,2,3] WU Yun-jie ZHANG Cong(State Key Laboratory of Virtual Reality Technology and Systems,Beihang University, Beijing 100191, China School of Automation Seienee and Eleetrieal Engineering, Beihang University, Beijing 100191, China Seienee and Teehnology on Aireraft Control Laboratory, Beihang University, Beijing 100191, China)

机构地区：[1]北京航空航天大学虚拟现实技术与系统国家重点实验室,北京100191 [2]北京航空航天大学自动化科学与电气工程学院,北京100191 [3]北京航空航天大学飞行器控制一体化技术重点实验室,北京100191

出　　处：《宇航学报》2016年第12期1441-1448,共8页Journal of Astronautics

基　　金：国家自然科学基金(91216304)

摘　　要：针对领弹—从弹编队构型的反舰导弹的末段协同制导,提出一体化位姿控制(ICPA)策略,将传统的位置跟踪控制和姿态稳定控制集成一体。建立便于一体化策略实施的串级型设计模型,在动态面控制的框架下设计一体化位姿控制算法,并通过Lyapunov方法证明其稳定性。从弹仅需获取领弹的位置信息,就能在确保自身姿态稳定的同时精确跟踪期望位置保持编队构型,而无需领弹的航向、速度、姿态等其他信息。总结一体化设计思想的本质:通过一个中间状态量建立质心方程和姿态方程之间的直接联系,集成出一个串级型设计模型,并针对其进行闭环算法设计。最后,通过仿真对所提出的一体化位姿控制策略及算法进行校验。An integrated control of position and attitude （ICPA） strategy is proposed by combining the traditional position tracking control and attitude stabilization control together for the cooperative terminal guidance of anti-ship missiles with a leader-follower structure. A cascade type design model, which is convenient for implementing the proposed integrated strategy, is established. The ICPA law is designed using dynamic control, and its stability is proven by Lyapunov method. Followers can accurately track the desired position while ensuring the stability of its own attitude by only obtaining the location information of the leader, but without others as course, speed and attitude. The essence of integrated design philosophy can be summarized that the direct relation between motion and dynamic equations is established by an intermediate state, and then the integrated closed loop algorithm is designed for the obtained cascade design model. Finally, a series of simulations are demonstrated to illustrate the effectiveness of the proposed ICPA strategy and algorithm.

关 键 词：反舰导弹 一体化位姿控制 主从编队 末制导段 动态面控制 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]