Closed Loop Guidance Algorithm for Solid Propellant Rocket*-Reference-Cited by-同舟云学术

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Closed Loop Guidance Algorithm for Solid Propellant Rocket*

Published:2013 Issue:19 Volume:46 Page:31-36
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Pietrobom Hilton Cleber,Filho Waldemar de Castro Leite

Publisher

Elsevier BV

Subject

General Medicine

Reference12 articles.

1. An optimal Q-guidance scheme for satellite launch vehicles;Bhat;Journal of Guidance,1987

2. Bianchi, S., Serraglia, F., and Barbagallo, D. (2005). A performance dispersion control strategy for vega launcher's third stage srm. 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.

3. Pointing algorithm - a strategy for orbit injection with uncontrolled last stage;Leite Filho,1994

4. Control system of brazilian launcher;Leite Filho,1999

5. ADAGA-Software To Trajectory Design And Guidance Assessment;Leite Filho,2003

Cited by 3 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. Explicit Midcourse Guidance Law for Multi-Stage Antiballistic Missile with Solid Propellant;2023 European Control Conference (ECC);2023-06-13

2. Instantaneous Impact Point Guidance with Coast Arcs for Solid Rockets;International Journal of Aerospace Engineering;2021-05-30

3. A Guidance Scheme for Air-launched Solid Launch Vehicle;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02

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