拦截机动目标的有限时间制导律及多弹协同制导律研究
目录
摘要 ........................................................................................................................... V II ABSTRACT .................................................................................................................. IX 第1章绪论 .. (17)
1.1课题背景及意义 (17)
1.2制导律的国内外研究现状 (19)
1.2.1经典制导律 (19)
1.2.2现代制导律 (20)
1.2.3几类常见制导律研究方向 (22)
1.2.4有限时间收敛制导律 (26)
1.3多导弹协同制导律的国内外研究现状 (28)
1.4本文的主要研究内容 (30)
第2章带终端攻击角约束的有限时间制导律 (32)
2.1引言 (32)
2.2导弹制导基础知识 (33)
2.2.1坐标系的定义 (33)
2.2.2坐标系之间的转换矩阵 (34)
2.2.3导弹和目标的运动方程 (34)
2.2.4导弹-目标相对运动信息计算公式 (35)
2.3平面内带终端攻击角约束的有限时间制导律 (36)
2.3.1平面内制导模型 (36)
2.3.2自适应滑模制导律设计 (38)
2.3.3基于有限时间干扰观测器的自适应滑模制导律 (42)
2.3.4仿真分析 (46)
2.4三维空间带终端攻击角约束的有限时间制导律 (52)
2.4.1三维空间的制导模型 (53)
2.4.2三维制导律设计 (55)
2.4.3仿真分析 (59)
2.5本章小结 (66)
第3章考虑自动驾驶仪动态特性及加速度饱和约束的制导律 (67)
3.1引言 (67)
3.2平面内考虑自动驾驶仪动态特性和加速度饱和约束的制导律 (68)
3.2.1平面内制导模型 (68)
3.2.2制导律设计 (69)
3.2.3仿真分析 (74)
XII
3.3三维空间内考虑自动驾驶仪动态特性和加速度饱和约束的有限时间制导律
(77)
3.3.1三维空间的制导模型 (77)
3.3.2三维制导律设计 (78)
3.3.3仿真分析 (87)
3.4本章小结 (91)
第4章带有终端攻击角约束的有限时间多导弹协同制导律 (93)
4.1引言 (93)
4.2平面内带终端攻击角约束的有限时间多导弹协同制导律 (94)
4.2.1平面内协同制导模型 (94)
4.2.2协同制导律设计 (97)
4.2.3仿真分析 (102)
4.3三维空间带终端攻击角约束的有限时间多导弹协同制导律 (105)
4.3.1三维空间的协同制导模型 (106)
4.3.2三维协同制导律设计 (108)
4.3.3仿真分析 (117)
4.4本章小结 (123)
第5章基于“领弹-从弹”协同策略的有限时间多导弹协同制导律 (124)
5.1引言 (124)
5.2基于“领弹-从弹”协同策略的协同制导模型 (125)
5.3基于SUPER-TWISTING算法的有限时间协同制导律 (128)
5.3.1协同制导律设计 (128)
5.3.2协同制导律的稳定性分析 (131)
5.4基于双层自适应SUPER-TWISTING算法的有限时间协同制导律 (135)
5.4.1协同制导律设计 (135)
5.4.2协同制导律的稳定性分析 (138)
5.5仿真分析 (141)
5.6本章小结 (146)
结论 (147)
参考文献 (150)
攻读博士学位期间发表的论文及其它成果 (164)
哈尔滨工业大学学位论文原创性说明及使用授权说明 (166)
致谢 (167)
个人简历 (168)
XIII
Contents
Abstract (In Chinese) ...................................................................................................... I Abstract (In English) .................................................................................................... I II Chapter 1 Introduction . (17)
1.1 Backkgroud and significance of dissertation (17)
1.2 Suvey of guidance laws (19)
1.2.1 Classical guidance laws (19)
1.2.2 Modern guidance laws (20)
1.2.3 Several kinds of common research directions for guidance law (22)
1.2.4 Finite-time convergence guidance laws (26)
1.3 Suvey of multiple missiles cooperative guidance laws (28)
1.4 Main contents of the dissertation (30)
Chapter 2 Finite-time guidance laws with terminal impact angle constraint (32)
2.1 Introduction (32)
2.2 Basic knowledge on missile guidance (36)
2.2.1 Definitions of coordinate systems (36)
2.2.2 Transfermation matrices between coordinate systems (38)
2.2.3 Motion equation of missile and target (42)
2.2.4 Formulas of target-missile relative motion information (46)
2.3 Finite-time guidance laws with terminal impact angle constraint in plane (36)
2.3.1 Guidance model in plane (36)
2.3.2 Design of adaptive sliding mode guidance law (38)
2.3.3 Design of finite-time observer-based adaptive sliding mode guidance law (42)
2.3.4 Simulation analysis (46)
2.4 Finite-time guidance law with terminal impact angle constraint in three-dimensional space (52)
2.4.1 Three-dimensional guidance model (53)
2.4.2 Design of three-dimensional guidance law (55)
2.4.3 Simulation analysis (59)
2.5 Conclusions (66)
XIV
Chapter 3 Guidance laws accounting for autopilot dynamics and acceleration saturation (67)
3.1 Introduction (67)
3.2 Guidance law accounting for autopilot dynamics and acceleration saturation in plane (68)
3.2.1 Guidance model in plane (68)
3.2.2 Design of guidance law (69)
3.2.3 Simulation analysis (74)
3.3 Finite-time guidance law accounting for autopilot dynamics and acceleration saturation in three-dimensional space (77)
3.3.1 Three-dimensional guidance model (77)
3.3.2 Design of three-dimensional guidance law (78)
3.3.3 Simulation analysis (87)
3.4 Conclusions (91)
Chapter 4 Finite-time cooperative guidance laws for multiple missiles with terminal impact angle constraint (93)
4.1 Introduction (93)
4.2 Finite-time cooperative guidance law for multiple missiles with terminal impact angle constraint in plane (94)
4.2.1 Cooperative guidance model in plane (94)
4.2.2 Design of cooperative guidance law (97)
4.2.3 Simulation analysis (102)
4.3 Finite-time cooperative guidance law for multiple missiles with terminal impact angle constraint in three-dimensional space (105)
4.3.1 Cooperative guidance model in three-dimensional space (106)
4.3.2 Design of three-dimensional cooperative guidance law (108)
4.3.3 Simulation analysis (117)
4.4 Conclusions (123)
Chapter 5 Finite-time cooperative guidance laws based on leader-follower cooperative strategies (124)
5.1 Introduction (124)
5.2 Cooperative guidance model based on leader-follower cooperative strategies (125)
5.3 Finite-time cooperative guidance laws using super-twisting algorithm (128)
XV
5.3.1 Design of cooperative guidance law (128)
5.3.2 Stability analysis of cooperative guidance law (131)
5.4 Finite-time cooperative guidance laws using adaptive dual-layer super-twisting algorithm (135)
5.4.1 Design of cooperative guidance law (135)
5.4.2 Stability analysis of cooperative guidance law (138)
5.5 Simulation analysis (141)
5.6 Conclusions (146)
Conclusions (147)
References (150)
Papers Published in the Period of Ph.D Education (164)
Statement of Copyright and Letter of Authorization (166)
Acknowledgement (167)
Resume (168)
XVI