1 |
LU P . Theory of fractional-polynomial powered descent guidance[J]. Journal of Guidance, Control, and Dynamics, 2020, 43 (3): 398- 409.
doi: 10.2514/1.G004556
|
2 |
WANG Z K , FU W X , FANG Y W , et al. Cooperative guidance law against highly maneuvering target with dynamic surrounding attack[J]. International Journal of Aerospace Engineering, 2021, 2021, 6623561.
|
3 |
XU H T , FOSSEN T I , SOARES C G . Uniformly semiglobally exponential stability of vector field guidance law and autopilot for path-following[J]. European Journal of Control, 2020, 53, 88- 97.
doi: 10.1016/j.ejcon.2019.09.007
|
4 |
KUMAR S R , SHIMA T . Cooperative nonlinear guidance stra-tegies for aircraft defense[J]. Journal of Guidance, Control and Dynamics, 2017, 40 (1): 124- 138.
doi: 10.2514/1.G000659
|
5 |
HUANG J S , ZHANG H B , TANG G J , et al. Extended diffe-rential geometric guidance law for intercepting maneuvering targets[J]. Journal of Systems Engineering and Electronics, 2018, 29 (5): 1046- 1057.
doi: 10.21629/JSEE.2018.05.15
|
6 |
YANG F , ZHANG K Q , YU L . Adaptive super-twisting algorithm-based nonsingular terminal sliding mode guidance law[J]. Journal of Control Science and Engineering, 2020, 2020, 1058347.
|
7 |
WANG C Y , DONG W , WANG J N , et al. Guidance law design with fixed-time convergent error dynamics[J]. Journal of Guidance, Control, and Dynamics, 2021, 44 (7): 1389- 1398.
doi: 10.2514/1.G005833
|
8 |
TIAN J Y , BAI X B , YANG H B , et al. Time-varying asymmetric barrier Lyapunov function-based impact angle control guidance law with field-of-view constraint[J]. IEEE Access, 2020, 8, 185346- 185359.
doi: 10.1109/ACCESS.2020.3030158
|
9 |
WEISS M , SHIMA T . Optimal linear-quadratic missile guidance laws with penalty on command variability[J]. Journal of Gui-dance, Control, and Dynamics, 2015, 38 (2): 226- 237.
doi: 10.2514/1.G000738
|
10 |
ZHANG T , LI J , WANG H J , et al. Attitude controller design with state constraints for kinetic kill vehicle based on barrier Lyapunov function[J]. Mathematical Problems in Engineering, 2018, 2018, 4397548.
|
11 |
ZHANG T , LI J , LI W M , et al. Prescribed performance neural control to guarantee tracking quality for near space kinetic kill vehicle[J]. Journal of Systems Engineering and Electro-nics, 2019, 30 (3): 573- 586.
doi: 10.21629/JSEE.2019.03.15
|
12 |
PEI P , WANG J . Near-optimal guidance with impact angle and velocity constraints using sequential convex programming[J]. Mathematical Problems in Engineering, 2019, 2019, 2065730.
|
13 |
郭建国, 韩拓, 周军, 等. 大气层外动能拦截器末制导律与能量优化方法[J]. 系统工程与电子技术, 2017, 39 (2): 376- 382.
|
|
GUO J G , HAN T , ZHOU J , et al. Terminal guidance law for exoatmospheric kill vehicle with energy optimization method[J]. Systems Engineering and Electronics, 2017, 39 (2): 376- 382.
|
14 |
PAL A , PANCHOLY A , DWIVEDI P N . Application of sub-optimal MPSC guidance for trajectory optimization of various aerospace vehicles with terminal angle constraint[J]. IFAC-PapersOnLine, 2018, 51 (1): 58- 63.
doi: 10.1016/j.ifacol.2018.05.011
|
15 |
CHO N , KIM Y , SHIN H S . Generalized formulation of linear nonquadratic weighted optimal error shaping guidance laws[J]. Journal of Guidance, Control, and Dynamics, 2020, 43 (6): 1- 11.
|
16 |
NO T S , COCHRAN J E , KIM E G . Bank-to-turn guidance law using Lyapunov function and nonzero effort miss[J]. Journal of Guidance, Control, and Dynamics, 2001, 24 (2): 255- 260.
doi: 10.2514/2.4736
|
17 |
LAM V C . Acceleration compensated zero effort miss guidance law[J]. Journal of Guidance, Control, and Dynamics, 2011, 30 (4): 1159- 1163.
|
18 |
YAN X D , SHI L . Robust intercept guidance law with predesigned zero-effort miss distance convergence for capturing maneuvering targets[J]. Journal of the Franklin Institute, 2020, 357 (2): 1118- 1136.
doi: 10.1016/j.jfranklin.2019.10.021
|
19 |
SHIMA T , IDAN M , GOLAN M O . Sliding-mode control for integrated missile autopilot guidance[J]. Journal of Guidance, Control, and Dynamics, 2006, 29 (2): 250- 260.
doi: 10.2514/1.14951
|
20 |
NEWMAN B . Strategic intercept midcourse guidance using modified zero effort miss steering[J]. Journal of Guidance, Control, and Dynamics, 1996, 19 (1): 107- 112.
doi: 10.2514/3.21586
|
21 |
崔彦凯, 梁晓庚, 王斐, 等. 弹道导弹助推段拦截最优制导律设计[J]. 飞行力学, 2011, 29 (1): 59- 62.
|
|
CUI Y K , LIANG X G , WANG F , et al. Design of optimal guidance law for interception ballistic miss during the boost phase[J]. Flight Dynamics, 2011, 29 (1): 59- 62.
|
22 |
李运迁, 齐乃明. 基于零控脱靶量的大气层内拦截弹制导律[J]. 宇航学报, 2010, 31 (7): 1768- 1774.
doi: 10.3873/j.issn.1000-1328.2010.07.011
|
|
LI Y Q , QI N M . A zero-effort miss distance-based guidance law for endoatmoshperic interceptor[J]. Journal of Astronautics, 2010, 31 (7): 1768- 1774.
doi: 10.3873/j.issn.1000-1328.2010.07.011
|
23 |
张浩, 张奕群, 张鹏飞. 拦截主动防御目标的微分对策制导律[J]. 系统工程与电子技术, 2021, 43 (5): 1335- 1345.
|
|
ZHANG H , ZHANG Y Q , ZHANG P F . Differential game guidance law for intercepting the active defense targets[J]. Systems Engineering and Electronics, 2021, 43 (5): 1335- 1345.
|
24 |
陈峰, 肖业伦, 陈万春. 基于零控脱靶量的大气层外超远程拦截制导[J]. 航空学报, 2009, 30 (9): 1583- 1589.
doi: 10.3321/j.issn:1000-6893.2009.09.005
|
|
CHEN F , XIAO Y L , CHEN W C . Guidance based on zero effort miss for super range exoatmospheric intercept[J]. Acta Aeronautic et Astronautica Sinica, 2009, 30 (9): 1583- 1589.
doi: 10.3321/j.issn:1000-6893.2009.09.005
|
25 |
陆诚, 崔朗福, 张庆振, 等. 基于线性重力差模型的拦截弹中制导技术[J]. 飞控与探测, 2020, 3 (3): 49- 56.
|
|
LU C , CUI L F , ZHANG Q Z , et al. Interceptor midcourse gui-dance technology based on linear gravity difference model[J]. Flight Control & Detection, 2020, 3 (3): 49- 56.
|
26 |
李玖阳, 胡敏, 王许煜, 等. 基于ALPSO算法的低轨卫星小推力离轨最优控制方法[J]. 系统工程与电子技术, 2021, 43 (1): 199- 207.
|
|
LI J Y , HU M , WANG X Y , et al. Optimal control method for low thrust deorbit of low earth orbit satellite based on ALPSO algorithm[J]. Systems Engineering and Electronics, 2021, 43 (1): 199- 207.
|
27 |
HU W J , WANG H , ZHOU J . Design of mid-course guidance law considering J2 perturbation for long range fuel exhaustion shutoff interceptor[J]. Journal of Astronautics, 2017, 38 (7): 694- 703.
|
28 |
SHSFERMAN V , SHIMA T . Linear quadratic laws for imposing a terminal intercept angle[J]. Journal of Guidance, Control, and Dynamics, 2008, 31 (5): 1400- 1412.
|
29 |
ZHANG H Q , TANG S J , GUO J . Cooperative near-space interceptor mid-course guidance law with terminal handover constraints[J]. Proceedings of the Institution of Mechanical Engineers, 2019, 233 (6): 1960- 1976.
|
30 |
MD A , CHOU H C , BOWLES J V . Near-optimal operation of dual-fuel launch vehicles[J]. Journal of Guidance, Control, and Dynamics, 1996, 19 (5): 1180- 1182.
|
31 |
LI Z , XIA Y , SU C Y , et al. Missile guidance law based on robust model predictive control using neural-network optimization[J]. IEEE Trans.on Neural Networks and Learning Systems, 2017, 26 (8): 1803- 1809.
|