火力与指挥控制2025，Vol.50Issue(5)：103-110,8.DOI:10.3969/j.issn.1002-0640.2025.05.015
基于L1-TECS算法领航模式无人机编队制导律设计
Guidance Law Design for UAV Formation in Navigation Mode Based on L1-TECS Algorithm
摘要
Abstract
In the formation flight mission,the follower UAV faces the dual challenges of external dis-turbances and sudden changes from the state of the leader UAV and should meet the strict requirements of anti-collision and keeping the formation.These factors provides higher technical challenges for trajec-tory tracking precision,speed control,rapid response,disturbance rejection capability,and speed adjust-ment.To meet the complex requirements of formation guidance and control,an innovative improvement and optimization is performed based on the classical framework of L1 lateral guidance law and total en-ergy control system.To address the impact of wind disturbances on the flight performance,a wind distur-bance motion model is established in conjunction with the control requirements of TECS.The simulation analyses and flight tests verify the true effectiveness of the proposed guidance law scheme.关键词
编队制导/L1算法/TECS/空速控制Key words
formation guidance/algorithm L1/TECS/airspeed control分类
军事科技引用本文复制引用
王惠方,李继广,陈欣,李二博,陈祉昂..基于L1-TECS算法领航模式无人机编队制导律设计[J].火力与指挥控制,2025,50(5):103-110,8.基金项目
国防科技重点实验室基金(6142101200108) （6142101200108）
陕西省自然科学青年基金(2021JQ-858) （2021JQ-858）
陕西省自然科学基金(2022JZ-37) （2022JZ-37）
西北工业大学国家重点实验室基金资助项目(202312-IFTKFKT-005) （202312-IFTKFKT-005）
