Proceedings of the 2014 International Conference on Mechatronics, Control and Electronic Engineering

Boost Trajectory Design for RBCC Engine

Authors
Zhichen Tan, Ke Zhang
Corresponding Author
Zhichen Tan
Available Online March 2014.
DOI
https://doi.org/10.2991/mce-14.2014.31How to use a DOI?
Keywords
Reentry; Hypersonic; Trajectory Optimization; RBCC; Gauss Pseudospectral Method
Abstract
With the development of the next generation of reusable aerospace vehicle, the technique of the Rocket Based Combined Cycle (RBCC) engine becomes increasingly significant and valuable. However, the performance of RBCC engine is coupled closely with the process of trajectory design. A model based on Radan Pseudospectral Optimal Method aiming at designing the boost trajectory is proposed in this paper. Two typical trajectories differing in variable and constant dynamic pressure constraints are simulated and compared. The constant dynamic pressure trajectory is designed simply with an acceptable optimal result. The feedback linearization algorithm to track the referent trajectory is analyzed and the simulated result shows its efficiency.
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Proceedings
2014 International Conference on Mechatronics, Control and Electronic Engineering (MCE-14)
Part of series
Advances in Intelligent Systems Research
Publication Date
March 2014
ISBN
978-94-62520-31-8
ISSN
1951-6851
DOI
https://doi.org/10.2991/mce-14.2014.31How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

TY  - CONF
AU  - Zhichen Tan
AU  - Ke Zhang
PY  - 2014/03
DA  - 2014/03
TI  - Boost Trajectory Design for RBCC Engine
BT  - 2014 International Conference on Mechatronics, Control and Electronic Engineering (MCE-14)
PB  - Atlantis Press
SP  - 143
EP  - 146
SN  - 1951-6851
UR  - https://doi.org/10.2991/mce-14.2014.31
DO  - https://doi.org/10.2991/mce-14.2014.31
ID  - Tan2014/03
ER  -