• DocumentCode
    1732578
  • Title

    Optimal control for consensus of spacecrafts cluster flight

  • Author

    Zhou Liang ; Luo Jianjun ; Zhang Bo

  • Author_Institution
    Sch. of Astronaut., Northwestern Polytech. Univ., Xi´an, China
  • fYear
    2013
  • Firstpage
    7185
  • Lastpage
    7190
  • Abstract
    This paper presents an optimal control method for consensus of spacecrafts cluster flight based on linear quadratic regulation (LQR). Firstly, we employ period-delayed errors as states of cooperative control and derive period-delayed errors dynamics of single spacecraft and the cluster of spacecrafts. Then, we converts the control problem of spacecrafts cluster flight periodically bounded relative motion into the consensus of period-delayed errors. We devise a feedback control law with a positive scalar called coupling gain. The notion of consensus region used in the consensus problem of multi-agent systems and the graph theory are analyzed. Considering the communication topology, we can select a suitable coupling gain according to the consensus region. Employing LQR-based optimal method, we can design the feedback control gain. So that the period-delayed errors of the spacecrafts cluster and semi-major axis of each spacecraft tend to consensus, which result in spacecrafts cluster emerging the global coordination swarming-like behavior. Numerical simulations are conducted verifying the effectiveness of the proposed LQR-based optimal control method for consensus of spacecrafts cluster flight.
  • Keywords
    aircraft control; control system synthesis; feedback; graph theory; linear quadratic control; numerical analysis; space vehicles; LQR; communication topology; consensus region notion; cooperative control; coupling gain; derive period-delayed errors dynamics; feedback control gain design; feedback control law; global coordination swarming-like behavior; graph theory; linear quadratic regulation; multi-agent systems; numerical simulations; optimal control method; period-delayed errors; periodically bounded relative motion; positive scalar; single spacecraft; spacecraft semi-major axis; spacecrafts cluster flight consensus; Aerodynamics; Couplings; Educational institutions; Electronic mail; Feedback control; Optimal control; Space vehicles; Consensus; Consensus Region; LQR; Period-delayed Errors; Spacecrafts Cluster Flight;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2013 32nd Chinese
  • Conference_Location
    Xi´an
  • Type

    conf

  • Filename
    6640702