Energy-Insensitive Guidance of Solid Motor Propelled Long Range Flight Vehicles Using MPSP and Dynamic Inversion-Reference-Cited by-同舟云学术

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Energy-Insensitive Guidance of Solid Motor Propelled Long Range Flight Vehicles Using MPSP and Dynamic Inversion

Published:2008 Issue:2 Volume:41 Page:14023-14028
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Kothari M.,Padhi R.

Publisher

Elsevier BV

Subject

General Medicine

Reference11 articles.

1. Guidance Evolution – A Personal Narrative;Battin;Journal of Guidance, Control and Dynamics,1982

2. Tactical and Strategic Missile Guidance;Zarchan;Proceeding in Astronautics and Aeronautics, AIAA Tactical Missile Series,1997

3. Padhi, R. (1999). An Optimal Explicit Guidance Scheme for Ballistic Missile with Solid Motors. Proceedings of AIAA Guidance, Navigation, and Control Conference. AIAA– 4140.

4. Applied Optimal Control;Bryson,1975

5. Padhi, R., M. Kothari and A. Kamath. Model Predictive Static Programming: A Promising Real-time Technique for Optimal Control Design. Technical Report: IISc/AE/LINCGODS/RP/2006/01.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Rendezvous Trajectory Control Laws in Low Earth Orbit Using Neural ODE for Continuous System Deep Learning;Transactions of the Society of Instrument and Control Engineers;2024

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