Close proximity asteroid operations using sliding control modes

Roberto Furfaro, Dario Cersosimo, Julie Bellerose

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Citations (Scopus)

Abstract

Due to their uncertain dynamical environment, close proximity operations around small celestial bodies are extremely challenging. In this paper, we show that the Multiple Sliding Surface Guidance (MSSG) algorithm, already proposed for autonomous asteroid pin-point guidance, can be extended to guide the transition of the spacecraft from any two desired states, including hovering, surface and orbital states. MSSG is based on Higher Order Sliding Mode (HOSM) control theory and takes advantage of the fact that the motion of the spacecraft around asteroids exists in a 2-sliding mode, i.e. The acceleration command appears at the second derivative of the defined sliding surface. The proposed algorithm is constructed by the proper concatenation of two sliding surfaces and takes advantage of the system's ability to reach the sliding surfaces in finite time. Importantly, the MSSG algorithm does not require either ground-based or on-board trajectory generation but computes an acceleration command that targets a specified state based on purely knowledge of the current and desired position and velocity. The classes of trajectories generated in this fashion are a function of the current and final states as well as of the guidance gains. Moreover, the controller is shown to be globally stable in the Lyapunov sense. MSSG is implemented in simulation scenarios comprising a variety of operations around a model asteroid, demonstrating the ability of the algorithm to guide the system between 1) two hovering states, 2) surface and hovering states and 3) surface to hovering. The MSSG algorithm is also shown to be able to shape the closed-loop trajectories to satisfy the requirements imposed by the need to execute a defined set of close-proximity operations.

Original languageEnglish (US)
Title of host publicationAdvances in the Astronautical Sciences
Pages455-470
Number of pages16
Volume143
StatePublished - 2012
Event22nd AAS/AIAA Space Flight Mechanics Meeting - Charleston, SC, United States
Duration: Feb 2 2012Feb 2 2012

Other

Other22nd AAS/AIAA Space Flight Mechanics Meeting
CountryUnited States
CityCharleston, SC
Period2/2/122/2/12

Fingerprint

Asteroids
Sliding mode control
asteroids
asteroid
sliding
proximity
hovering
trajectory
Trajectories
trajectories
commands
Spacecraft
spacecraft
celestial bodies
control theory
Control theory
controllers

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Furfaro, R., Cersosimo, D., & Bellerose, J. (2012). Close proximity asteroid operations using sliding control modes. In Advances in the Astronautical Sciences (Vol. 143, pp. 455-470)

Close proximity asteroid operations using sliding control modes. / Furfaro, Roberto; Cersosimo, Dario; Bellerose, Julie.

Advances in the Astronautical Sciences. Vol. 143 2012. p. 455-470.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Furfaro, R, Cersosimo, D & Bellerose, J 2012, Close proximity asteroid operations using sliding control modes. in Advances in the Astronautical Sciences. vol. 143, pp. 455-470, 22nd AAS/AIAA Space Flight Mechanics Meeting, Charleston, SC, United States, 2/2/12.
Furfaro R, Cersosimo D, Bellerose J. Close proximity asteroid operations using sliding control modes. In Advances in the Astronautical Sciences. Vol. 143. 2012. p. 455-470
Furfaro, Roberto ; Cersosimo, Dario ; Bellerose, Julie. / Close proximity asteroid operations using sliding control modes. Advances in the Astronautical Sciences. Vol. 143 2012. pp. 455-470
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