𝔖 Bobbio Scriptorium

✦ LIBER ✦

Advanced guidance laws for acceleration-constrained missile, randomly maneuvering target and noisy measurements

✍ Scribed by Rusnak, I.

Book ID: 118268966
Publisher: IEEE
Year: 1996
Tongue: English
Weight: 821 KB
Volume: 32
Category: Article
ISSN: 0018-9251
DOI: 10.1109/7.481287

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Optimal guidance for acceleration constr

Optimal guidance for acceleration constrained missile and maneuvering target

✍ Rusnak, I.; Meir, L. 📂 Article 📅 1990 🏛 IEEE 🌐 English ⚖ 440 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics AIAA Guidance, Navigation, and Control Conference and Exhibit - Austin, Texas ()] AIAA Guidance, Navigation, and Control Conference and Exhibit - Optimal Guidance Laws with Uncertain Time-of-Flight Against Maneuvering Target and Noisy Measurements

✍ Rusnak, Ilan 📂 Article 📅 2003 🏛 American Institute of Aeronautics and Astronautics ⚖ 440 KB

[IEEE 2011 2nd International Conference

[IEEE 2011 2nd International Conference on Control, Instrumentation, and Automation (ICCIA) - Shiraz, Iran (2011.12.27-2011.12.29)] The 2nd International Conference on Control, Instrumentation and Automation - Backstepping guidance law design for missile against maneuvering targets

✍ Moosapour, S. H.; Bagherzadeh, M.; Alizadeh, G.; Ghaemi, S. 📂 Article 📅 2011 🏛 IEEE ⚖ 261 KB

[IEEE WCICA 2000. Proceedings of the 3rd

[IEEE WCICA 2000. Proceedings of the 3rd World Congress on Intelligent Control and Automation - Hefei, China (28 June-2 July 2000)] Proceedings of the 3rd World Congress on Intelligent Control and Automation (Cat. No.00EX393) - Studying and accomplishing a new guidance law for homing missile attacking maneuvering target

✍ Xiaohu Wang, ; Minglian Zhang, 📂 Article 📅 2000 🏛 IEEE ⚖ 311 KB