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Aerospace, v.9 no.1, 2022년, pp.32 -
Raza, Ali , Wang, Hua
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This paper presents a two-phase guidance and control algorithm to extend the range and improve the impact point accuracy of a 122-mm rocket using a fixed canards trajectory correction fuze. The guidance algorithm consists of a unique glide and correction phase of the rocket trajectory that is activa...
Rogers, Jonathan, Costello, Mark. Design of a Roll-Stabilized Mortar Projectile with Reciprocating Canards. Journal of guidance, control, and dynamics : a publication of the American Institute of Aeronautics and Astronautics devoted to the technology of dynamics and control, vol.33, no.4, 1026-1034.
Chang, Sijiang, Wang, Zhongyuan, Liu, Tiezheng. Analysis of Spin-Rate Property for Dual-Spin-Stabilized Projectiles with Canards. Journal of spacecraft and rockets, vol.51, no.3, 958-966.
Cooper, Gene, Fresconi, Frank, Costello, Mark. Flight Stability of an Asymmetric Projectile with Activating Canards. Journal of spacecraft and rockets, vol.49, no.1, 130-135.
Theodoulis, Spilios, Gassmann, Vincent, Wernert, Philippe, Dritsas, Leonidas, Kitsios, Ioannis, Tzes, Anthony. Guidance and Control Design for a Class of Spin-Stabilized Fin-Controlled Projectiles. Journal of guidance, control, and dynamics : a publication of the American Institute of Aeronautics and Astronautics devoted to the technology of dynamics and control, vol.36, no.2, 517-531.
Elsaadany, Ahmed, Wen-jun, Yi. Accuracy Improvement Capability of Advanced Projectile Based on Course Correction Fuze Concept. The Scientific World Journal, vol.2014, 273450-.
Theodoulis, S., Seve, F., Wernert, P.. Robust gain-scheduled autopilot design for spin-stabilized projectiles with a course-correction fuze. Aerospace science and technology, vol.42, 477-489.
Gao, Min, Zhang, Yongwei, Yang, Suochang. Firing Control Optimization of Impulse Thrusters for Trajectory Correction Projectiles. International journal of aerospace engineering, vol.2015, 1-11.
Jacewicz Monte-Carlo Based Lateral Thruster Parameters Optimization for 122 mm Rocket Automation 2020: Towards Industry of the Future 2020 125
Yang, Shu. Impact-Point-Based Guidance of a Spinning Artillery Rocket Using Canard Cyclic Control. Journal of guidance, control, and dynamics : a publication of the American Institute of Aeronautics and Astronautics devoted to the technology of dynamics and control, vol.43, no.10, 1975-1982.
10.1155/2001/615748
Costello Potential Field Artillery Projectile Improvement Using Movable Canards 1997
Liu, Xu-dong, Li, Dong-guang, Shen, Qiang. Swerving Orientation of Spin-Stabilized Projectile for Fixed-Cant Canard Control Input. Mathematical problems in engineering, vol.2015, 1-11.
Yin, Tingting, Jia, Fangxiu, Yu, Jiyan. Research on Roll Control System for Fixed Canard Rudder of the Dual-Spin Trajectory Correction Projectile. Wireless personal communications, vol.103, no.1, 83-98.
Cheng,, Shen,, Deng,, Deng,. Novel Aiming Method for Spin-Stabilized Projectiles with a Course Correction Fuze Actuated by Fixed Canards. Electronics, vol.8, no.10, 1135-.
Zhu, Dalin, Tang, Shengjing, Guo, Jie, Chen, Rui. Flight stability of a dual-spin projectile with canards. Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, vol.229, no.4, 703-716.
Slegers, Nathan. Predictive Control of a Munition Using Low-Speed Linear Theory. Journal of guidance, control, and dynamics : a publication of the American Institute of Aeronautics and Astronautics devoted to the technology of dynamics and control, vol.31, no.3, 768-775.
10.2514/6.2004-5359
Fresconi, Frank. Guidance and Control of a Projectile with Reduced Sensor and Actuator Requirements. Journal of guidance, control, and dynamics : a publication of the American Institute of Aeronautics and Astronautics devoted to the technology of dynamics and control, vol.34, no.6, 1757-1766.
Fresconi, Frank, Cooper, Gene, Costello, Mark. Practical Assessment of Real-Time Impact Point Estimators for Smart Weapons. Journal of aerospace engineering, vol.24, no.1, 1-11.
ZHANG, Xin, YAO, Xiaoxian, ZHENG, Qiushi. Impact point prediction guidance based on iterative process for dual-spin projectile with fixed canards. Chinese journal of aeronautics, vol.32, no.8, 1967-1981.
Hainz III, Leonard C., Costello, Mark. Modified Projectile Linear Theory for Rapid Trajectory Prediction. Journal of guidance, control, and dynamics : a publication of the American Institute of Aeronautics and Astronautics devoted to the technology of dynamics and control, vol.28, no.5, 1006-1014.
Zipfel Modeling and Simulation of Aerospace Vehicle Dynamics 2007
10.2514/6.2002-4416
Li, Jie Min, He, Guang Lin, Guo, Hao Yang. A Study on the Aerodynamic Characteristics for a Two-Dimensional Trajectory Correction Fuze. Applied mechanics and materials, vol.703, 370-375.
Tun, N L, Thuri, M, Minnzinoo,, Li, Z. Aerodynamic Coefficients Prediction for 122 mm Rocket by Using Computational Fluid Dynamics. IOP conference series. Materials science and engineering, vol.816, 012010-.
10.21608/asat.2009.23742
Fresconi, F, Plostins, P. Control mechanism strategies for spin-stabilized projectiles. Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, vol.224, no.9, 979-991.
Wang, Zhong-yuan, Chang, Si-jiang. Impact Point Prediction and Analysis of Lateral Correction Analysis of Two-Dimensional Trajectory Correction Projectiles. Defence technology, vol.9, no.1, 48-52.
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