TY - JOUR
T1 - Orbit control scheme of the terminal course of side window detection kinetic kill vehicle
AU - Wang, Yang
AU - Zhou, Jun
AU - Zhao, Bin
AU - You, Yu Hua
N1 - Publisher Copyright:
© 2016, Editorial Dept. of JSRT. All right reserved.
PY - 2016/8/1
Y1 - 2016/8/1
N2 - In terms of the orbit control problem of the terminal course of side window detection kinetic kill vehicle(SWDKKV), this article puts forward a new rail control scheme based on the variable structure control theory. First of all, an orbit control model under three dimensional space was established after considering the restraints of side window. Subsequently, a new type of sliding mode surface with variable structure was presented based on such features of side window detection kinetic kill vehicle as being only able to output constant switching thrust and having directional attitude constraints, and a bang-bang type of orbit control scheme suitable for terminal intercept was designed. Lyapunov stability theory was adopted to strictly prove the stability of the proposed methods. In order to reduce jet consumption, a sliding dead zone was designed and the value range of parameters in sliding dead zone which can ensure hitting accuracy was studied. Simulation results show that the designed orbit control scheme can meet the accuracy requirements while sliding dead zone can reduce jet consumption.
AB - In terms of the orbit control problem of the terminal course of side window detection kinetic kill vehicle(SWDKKV), this article puts forward a new rail control scheme based on the variable structure control theory. First of all, an orbit control model under three dimensional space was established after considering the restraints of side window. Subsequently, a new type of sliding mode surface with variable structure was presented based on such features of side window detection kinetic kill vehicle as being only able to output constant switching thrust and having directional attitude constraints, and a bang-bang type of orbit control scheme suitable for terminal intercept was designed. Lyapunov stability theory was adopted to strictly prove the stability of the proposed methods. In order to reduce jet consumption, a sliding dead zone was designed and the value range of parameters in sliding dead zone which can ensure hitting accuracy was studied. Simulation results show that the designed orbit control scheme can meet the accuracy requirements while sliding dead zone can reduce jet consumption.
KW - Kinetic kill vehicle
KW - Orbit control scheme
KW - Side window detection
KW - Sliding dead zone
KW - Sliding mode control
KW - Terminal guidance
UR - http://www.scopus.com/inward/record.url?scp=85014315252&partnerID=8YFLogxK
U2 - 10.7673/j.issn.1006-2793.2016.04.025
DO - 10.7673/j.issn.1006-2793.2016.04.025
M3 - 文章
AN - SCOPUS:85014315252
SN - 1006-2793
VL - 39
SP - 588
EP - 593
JO - Guti Huojian Jishu/Journal of Solid Rocket Technology
JF - Guti Huojian Jishu/Journal of Solid Rocket Technology
IS - 4
ER -