Modelling and control of satellite formations

[1]  R. Sedwick,et al.  High-Fidelity Linearized J Model for Satellite Formation Flight , 2002 .

[2]  R. Melton Time-Explicit Representation of Relative Motion Between Elliptical Orbits , 2000 .

[3]  Frederick H. Lutze,et al.  Second-Order Relative Motion Equations , 2003 .

[4]  Jay W. Middour Along track formationkeeping for satellites with low eccentricity , 1992 .

[5]  Fumin Zhang,et al.  Formation dynamics under a class of control laws , 2002, Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301).

[6]  F. Bauer,et al.  Spacecraft Formation Flying Maneuvers Using Linear-Quadratic Regulation with No Radial Axis Inputs , 2001 .

[7]  Vikram Kapila,et al.  Adaptive Nonlinear Control of Multiple Spacecraft Formation Flying , 2000 .

[8]  J. How,et al.  Relative Dynamics and Control of Spacecraft Formations in Eccentric Orbits , 2000 .

[9]  H. Schaub,et al.  Impulsive Feedback Control to Establish Specific Mean Orbit Elements of Spacecraft Formations , 2001 .

[10]  G. C. Knollman,et al.  RELATIVE TRAJECTORIES OF OBJECTS EJECTED FROM A NEAR SATELLITE , 1963 .

[11]  Jonathan P. How,et al.  Co‐ordination and control of distributed spacecraft systems using convex optimization techniques , 2002 .

[12]  Maurice L. Anthony,et al.  Rendezvous Problem for Nearly Circular Orbits , 1965 .

[13]  K. Yamanaka,et al.  New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit , 2002 .

[14]  S. R. Vadali,et al.  An intelligent control concept for formation flying satellites , 2002 .

[15]  K. Alfriend,et al.  State Transition Matrix of Relative Motion for the Perturbed Noncircular Reference Orbit , 2003 .

[16]  LARGE-ANGLE KINEMATICS FOR THE CONTROL OF SATELLITE RELATIVE MOTION , 2002 .

[17]  Kyle T. Alfriend,et al.  Hybrid Cartesian and Orbit Element Feedback Law for Formation Flying Spacecraft , 2000 .

[18]  J. P. De Vries,et al.  ELLIPTIC ELEMENTS IN TERMS OF SMALL INCREMENTS OF POSITION AND VELOCITY COMPONENTS , 1963 .

[19]  H. London,et al.  SECOND APPROXIMATION TO THE SOLUTION OF THE RENDEZVOUS EQUATIONS , 1963 .

[20]  T. Carter,et al.  Fuel-Optimal Rendezvous Near a Point in General Keplerian Orbit , 1987 .

[21]  T. Carter State Transition Matrices for Terminal Rendezvous Studies: Brief Survey and New Example , 1998 .

[22]  Srinivas R. Vadali,et al.  Fuel Optimal Control for Formation Flying of Satellites , 1999 .