TY - GEN
T1 - Optimal Control for Deployment of Charged Spacecraft Formation Flying Based LQR
AU - Artitthang, Peerawat
AU - Lin, Mingpei
AU - Xu, Ming
N1 - Publisher Copyright:
© 2019 IEEE.
PY - 2019/8
Y1 - 2019/8
N2 - The properties of coulomb force (CF) that nearly propellantless and exhaust plume contaminatless compared to the conventional chemical liquid propulsion thrusters (e.g., micro PPT, FEEP...etc.), make it attractive use for the close formation flying of the spacecraft at high Earth orbit (HEO). This paper presents the charged feedback controller using the optimal control based on the Linear Quadratic Regulator (LQR) method. The interaction between the CF that generated from charged sphere devices on the Target and Chase crafts are exploited to deploy the Chaser from the Target. Finally, the simulation results showed the effectiveness coulomb feedback-based LQR controller can be efforted the initial position of the Chaser entry to the design orbit as expected. The command force expenditure is on the order of -9 to 48 milli-Newton, in which the magnitude of coulomb charged has bounded.
AB - The properties of coulomb force (CF) that nearly propellantless and exhaust plume contaminatless compared to the conventional chemical liquid propulsion thrusters (e.g., micro PPT, FEEP...etc.), make it attractive use for the close formation flying of the spacecraft at high Earth orbit (HEO). This paper presents the charged feedback controller using the optimal control based on the Linear Quadratic Regulator (LQR) method. The interaction between the CF that generated from charged sphere devices on the Target and Chase crafts are exploited to deploy the Chaser from the Target. Finally, the simulation results showed the effectiveness coulomb feedback-based LQR controller can be efforted the initial position of the Chaser entry to the design orbit as expected. The command force expenditure is on the order of -9 to 48 milli-Newton, in which the magnitude of coulomb charged has bounded.
KW - LQR
KW - coulomb feedback control system
KW - coulomb formation flying
KW - formation deployment
UR - https://www.scopus.com/pages/publications/85083636382
U2 - 10.1109/ICCSSE.2019.00015
DO - 10.1109/ICCSSE.2019.00015
M3 - 会议稿件
AN - SCOPUS:85083636382
T3 - Proceedings - 5th International Conference on Control Science and Systems Engineering, ICCSSE 2019
SP - 35
EP - 39
BT - Proceedings - 5th International Conference on Control Science and Systems Engineering, ICCSSE 2019
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 5th International Conference on Control Science and Systems Engineering, ICCSSE 2019
Y2 - 14 August 2019 through 16 August 2019
ER -