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An Autonomous and Dependable Formation Flying Technique

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Space Ops 2004, Montreal, QC, Canada. Facts about micro satellites & clusters. Faster production cycle and less expensive than large satellite ... – PowerPoint PPT presentation

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Title: An Autonomous and Dependable Formation Flying Technique


1
An Autonomous and Dependable Formation Flying
Technique
  • Sergey Butenkov Taganrog University, RU
  • Oleg Semery Taganrog University, RU
  • Siamak Tafazoli CSA, CA
  • Space Ops 2004, Montreal, QC, Canada

2
Facts about micro satellites clusters
  • Faster production cycle and less expensive than
    large satellite
  • Distribute functions of single large satellite
    among several small cooperative units
  • Multi sensors, various missions
  • A cluster can synthesize larger aperture
    providing much better image resolution

3
Motivation
  • To enable orbit corrections during formation
    flying
  • To provide an autonomous and dependable on-board
    control for orbit maneuvering, formation flying
    reconfiguration and deconfiguration

4
Our approach
  • Consider reduced dynamic equations
  • Obtain the analytical form for the on-board
    controller
  • Use the on-board controller for maneuvers

5
Main results
  • Provide orbit perturbation compensation by
    on-board controller
  • Simple and fast on-board controller
  • Control techniques will provide a fuel-efficient
    way for maneuvers

6
Common satellite controller structure
7
Relevant coordinate frames
8
Reconfiguration Maneuvers
 
9
Results Orbit transfer maneuver
Attraction to the target orbit with the
oscillatory movement
Phase trajectory in (r,r) plane for the
oscillatory movement
10
Results 2-satellite formation flying maneuver
2-satellite formation flying maneuvers
2-satellite formation flying maneuvers
2-satellite formation flying maneuvers
11
Results 4-satellite reconfiguration maneuver
2-satellite formation flying maneuvers
2-satellite formation flying maneuvers
2-satellite formation flying maneuvers
12
Conclusion and future work
  • Techniques presented in this paper, based on
    optimal synergetics, may be useful for many
    different engineering applications
  • Consider satellites with limited control forces
  • Include environmental perturbations
  • Consider attitude control during maneuvers
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