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
gravity, atmospheric drag, guidance, PBV maneuvers, and threat complex deployment. Using a da- tabase of representative missiles, threats from MDA’s Adversary Capabilities Document (ACD2006), or custom MDT models, trajectories and range contours can be analyzed in STK Custom BallistiC missile ...
The paper focuses on the reinforcement learning adaptive risk-sensitive fault-tolerant integrated guidance and control (IGC) for a class of skid-to-turn (S... Z Wang,Y Hao - 《Nonlinear Dynamics》 被引量: 0发表: 2024年 加载更多研究点推荐 R&D Cost Estimation Model Missile System cost estimat...
3.2. Missile guidance law Air-to-air missile uses proportional navigation law of three-dimensional space. In proportional navigation law, in speed coordinates, the command acceleration of air-to-air missile is(5)ay=-k1|ṙ|q̇yaz=-k2|ṙ|q̇zwhere k1 and k2 are proportional coefficie...
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
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: 95 收藏 报错 分享 全部来源 求助全文 AIAA 相似文献 参考文献Variable Stiffness Adaptive Structures utilizing Hydraulically Pressurized ...
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...
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 ...
guidance and control system via reduced-order ESO. ISA Transactions (2015), http://dx.doi/10.1016/j.isatra.2015.02.013i ISA Transactions ∎ (∎∎∎∎) ∎∎∎–∎∎∎ model with uncertainties is formulated, where an adaptive non- linear IGC approach combined with back-stepp...