TY - JOUR
T1 - Review of the control of low dynamic vehicles in near space
AU - Guo, Jianguo
AU - Zhou, Jun
PY - 2014
Y1 - 2014
N2 - The latest development and tendency of the flight control systems for low dynamic vehicles in the near space is analyzed and summarized in view of the new problems in the research of the control technology. Firstly, based on the characteristics of the vehicles, including near-space airships and stratospheric balloons in different flight environments of stratosphere and troposphere, the basic problems and key technologies of the low dynamic vehicles are generalized. Secondly, special attention is paid to the following areas in flight control system design for low dynamic vehicles: the servo control system design, mathematical models, attitude control, station-keeping control, velocity control, trajectory optimization, path tracking control, ascent control, descent control, pressure control, and control strategies in applying all kinds of control approaches. Finally, some key issues are proposed which deserve more attention of the researchers for their solution on the basis of the progress of existing research in relevant fields.
AB - The latest development and tendency of the flight control systems for low dynamic vehicles in the near space is analyzed and summarized in view of the new problems in the research of the control technology. Firstly, based on the characteristics of the vehicles, including near-space airships and stratospheric balloons in different flight environments of stratosphere and troposphere, the basic problems and key technologies of the low dynamic vehicles are generalized. Secondly, special attention is paid to the following areas in flight control system design for low dynamic vehicles: the servo control system design, mathematical models, attitude control, station-keeping control, velocity control, trajectory optimization, path tracking control, ascent control, descent control, pressure control, and control strategies in applying all kinds of control approaches. Finally, some key issues are proposed which deserve more attention of the researchers for their solution on the basis of the progress of existing research in relevant fields.
KW - Airships
KW - Attitude control
KW - Flight control system
KW - Mathematical model
KW - Stratospheric balloon
KW - Trajectory
UR - https://www.scopus.com/pages/publications/84897138753
U2 - 10.7527/S1000-6893.2013.0435
DO - 10.7527/S1000-6893.2013.0435
M3 - 文献综述
AN - SCOPUS:84897138753
SN - 1000-6893
VL - 35
SP - 320
EP - 331
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 2
ER -