A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles
Joint Authors
Source
International Journal of Aerospace Engineering
Issue
Vol. 2016, Issue 2016 (31 Dec. 2016), pp.1-11, 11 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2016-07-21
Country of Publication
Egypt
No. of Pages
11
Abstract EN
This study proposes a multiconstrained ascent guidance method for a solid rocket-powered launch vehicle, which uses a hypersonic glide vehicle (HGV) as payload and shuts off by fuel exhaustion.
First, pseudospectral method is used to analyze the two-stage launch vehicle ascent trajectory with different rocket ignition modes.
Then, constraints, such as terminal height, velocity, flight path angle, and angle of attack, are converted into the constraints within height-time profile according to the second-stage rocket flight characteristics.
The closed-loop guidance method is inferred by different spline curves given the different terminal constraints.
Afterwards, a thrust bias energy management strategy is proposed to waste the excess energy of the solid rocket.
Finally, the proposed method is verified through nominal and dispersion simulations.
The simulation results show excellent applicability and robustness of this method, which can provide a valuable reference for the ascent guidance of solid rocket-powered launch vehicles.
American Psychological Association (APA)
Chen, Si-Yuan& Xia, Qun-Li. 2016. A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles. International Journal of Aerospace Engineering،Vol. 2016, no. 2016, pp.1-11.
https://search.emarefa.net/detail/BIM-1105012
Modern Language Association (MLA)
Chen, Si-Yuan& Xia, Qun-Li. A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles. International Journal of Aerospace Engineering No. 2016 (2016), pp.1-11.
https://search.emarefa.net/detail/BIM-1105012
American Medical Association (AMA)
Chen, Si-Yuan& Xia, Qun-Li. A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles. International Journal of Aerospace Engineering. 2016. Vol. 2016, no. 2016, pp.1-11.
https://search.emarefa.net/detail/BIM-1105012
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1105012