In this brief, the utilization of robust model-based predictive control is investigated for the problem of missile interception. Treating the target acceleration as a bounded disturbance, novel guidance law using model predictive control is developed by incorporating missile inside constraints. The combine...
Multimodel LQ Pursuer-Evader Game for Missile Guidance - ScienceDirectdoi:10.1016/s1474-6670(17)30539-6Carlos Jimenez GallegosS. AlexanderG. PoznyakIFAC Proceedings Volumes
According to the above analysis, the integrated model of the guidance and autopilot system for homing missiles can be written as(10)ẋ0=f0(x0)+g0(t)x1#+d0(t)ẋ1=f1(x1)+g1(ϑ,x1)x2+d1(t)ẋ2=f2(x1,x2)+g2(t)u+d2(t)In this paper, the uncertainties d0(t), d...
Cooperative Multiple Model Adaptive Guidance for an Aircraft Defending Missile* - AIAA Guidance, Navigation, and Control Conference (AIAA) 来自 AIAA 喜欢 0 阅读量: 93 收藏 报错 分享 全部来源 求助全文 AIAA 相似文献 参考文献Hybrid state estimation and model-set design of invariable-structure semi-...
A 3-DOF point mass kinematic model of an ideal proportional navigation guidance missile written entirely in Python 3. Capable of creating trajectory files compatible with the pyThreeD program provided herein and the threeD program available at https://ww
3D Guidance Model for Anti-ship Missile Penetration 来自 Semantic Scholar 喜欢 0 阅读量: 16 作者:GU Wen-Jina,RC Zhang,HC Zhao 摘要: It is an effective method to applying three-dimensional (3D) variation trajectory guidance law for improving penetration capability of super-sonic anti-ship ...
6. Conclusion -e main innovations and contributions of this paper are as follows: (1) It is the first time to publicly evaluate the entire system of MEMLS to provide basis and guidance for the design and improvement of the system. (2) -e paper is based on the ADC model and uses EWM...
variationsofaerodynamicsparametersinguidanceandcontrolloopareviewedasuncertainties,whichareestimatedandcompensatedbydesignedmodel-assistedreduced-orderextendedstateobserver(ESO).Second,basedontheprincipleofactivedisturbancerejectioncontrol(ADRC),enhancedfeedbacklinearization(FL)basedcontrollawisimplementedfortheIGCmodelusingthe...
A new approach to maneuvering target tracking using the Sliding Mode Observer theory, in the specific context of homing missile guidance, is developed. This scheme requires a priori information about the target acceleration bounds alone, and there is no need for a dynamic model to represent the ...
内容提示: Integrated Sliding Mode Guidance and Controlfor a Missile with On–Off ActuatorsAmir Koren∗and Moshe Idan†Technion—Israel Institute of Technology, 32000 Haifa, IsraelandOded M. Golan‡RAFAEL, 31021 Haifa, IsraelDOI: 10.2514/1.31328A sliding mode controller was recently introduced ...