TY - GEN
T1 - Research on multi-model of hypersonic vehicle based on bifurcation theory
AU - Su, Erlong
AU - Min, Changwan
AU - Xiao, Zhen
AU - Yang, Ming
AU - Wang, Ying
AU - Luo, Jianjun
N1 - Publisher Copyright:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2017
Y1 - 2017
N2 - The bifurcation theory was employed to divide the multi-model of hypersonic vehicle. The eigenvalue topologies of nonlinear dynamics of hypersonic vehicle were obtained through applying the continuation method, and the relation between the eigenvalue and dynamics of sub-model was established. Based on the variation of dynamic characteristics, the multi-models were successfully divided. Firstly, the relation between eigenvalue and dynamics of sub-model was established, and the topologies of eigenvalue of longitudinal model (short period mode) was being computed and the relation between eigenvalue and sub-model dynamics was given, after that the three sub-models for longitudinal model were obtained; Correspondingly, for the lateral dynamic model, the topologies of eigenvalue corresponding to Dutch roll mode and roll subsistence mode were computed and the lateral model was divided into 6 sub-models finally. Lastly, the eigenvalue topologies for 5 order coupled model was computed and coupled dynamic model was divided into 4 sub-models. The results above can provide the important information for strategies of control and switch of the sub-models as well as controller design for hypersonic vehicle.
AB - The bifurcation theory was employed to divide the multi-model of hypersonic vehicle. The eigenvalue topologies of nonlinear dynamics of hypersonic vehicle were obtained through applying the continuation method, and the relation between the eigenvalue and dynamics of sub-model was established. Based on the variation of dynamic characteristics, the multi-models were successfully divided. Firstly, the relation between eigenvalue and dynamics of sub-model was established, and the topologies of eigenvalue of longitudinal model (short period mode) was being computed and the relation between eigenvalue and sub-model dynamics was given, after that the three sub-models for longitudinal model were obtained; Correspondingly, for the lateral dynamic model, the topologies of eigenvalue corresponding to Dutch roll mode and roll subsistence mode were computed and the lateral model was divided into 6 sub-models finally. Lastly, the eigenvalue topologies for 5 order coupled model was computed and coupled dynamic model was divided into 4 sub-models. The results above can provide the important information for strategies of control and switch of the sub-models as well as controller design for hypersonic vehicle.
KW - Bifurcation theory
KW - Hypersonic vehicle
KW - Multi-model
KW - Nonlinear loss of stability
UR - http://www.scopus.com/inward/record.url?scp=85017566937&partnerID=8YFLogxK
M3 - 会议稿件
AN - SCOPUS:85017566937
SN - 9781624104633
T3 - 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
BT - 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
Y2 - 6 March 2017 through 9 March 2017
ER -