Astronomy and Astrophysics – Astronomy
Scientific paper
Jun 1998
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1998jass...15..235p&link_type=abstract
Journal of Astronomy and Space Sciences, vol. 15, no. 1, p. 235-244.
Astronomy and Astrophysics
Astronomy
Scientific paper
The solutions of orbital maneuver problem using the sliding mode control in the presence of the earth gravitational perturbations is obtained. Especially, the optimization of consuming fuel for maneuver is performed. The impulsive solution to Lambert's problem using the combined equation method to minimize total Delta V is used for the desired orbit and the maneuver times. Two-step sliding mode control method is introduced for satisfying the boundary conditions of finite-thrust rendezvous problem at the end of maneuver time. Using the new approach to the orbit maneuver problem, two-step sliding mode control, orbit maneuvers are processed. The solutions to a rendezvous using the optimal control are obtained, and they are compared to the results by two-step sliding control. According to the new approach for orbit maneuver, the thrust-coast-thrust type controller is obtained to make satellite to track desired Lambert's orbit, and the total Delta V required for maneuver is resonable in comparison with the impulsive solution to Lambert's problem. The final state variables, also are close to the boundary conditions at the end of maneuver times.
Choi Kyu-Hong
Lee Sanguk
Park Jong-Uk
No associations
LandOfFree
Orbital Maneuver using Two-Step Sliding Mode Control does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with Orbital Maneuver using Two-Step Sliding Mode Control, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Orbital Maneuver using Two-Step Sliding Mode Control will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1333326