A Closed-loop Optimal Feedback Guidance Method of Reentry Phase for Hypersonic Glide Vehicle

A closed-loop optimal feedback guidance method based on online trajectory optimization and optimal feedback control was proposed for reentry guidance of hypersonic glide vehicle with multi constraints. The mathematical model of the reentry guidance problem with complex multi constraints was establis...

وصف كامل

التفاصيل البيبلوغرافية

الحاوية / القاعدة:	Kongzhi Yu Xinxi Jishu
المؤلفون الرئيسيون:	LIAO Yuxin, LI Jun, LI Xiaodong
التنسيق:	مقال
اللغة:	الصينية
منشور في:	Editorial Office of Control and Information Technology 2018-01-01
الموضوعات:	hypersonic glide vehicle reentry guidance trajectory optimization optimal feedback control
الوصول للمادة أونلاين:	http://ctet.csrzic.com/thesisDetails#10.13889/j.issn.2096-5427.2018.06.013