Constant thrust collision avoidance maneuver under thruster failure

Statistics – Computation

Scientific paper

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

Scientific paper

In this paper, the collision avoidance maneuver under the chaser's thruster failure in radial direction is investigated. First, based on the vision measurement, the relative position parameters of the target spacecraft are obtained and the target maneuvre positions are calculated through the isochronous interpolation method. Then, by using coupling effects, the thrusters working time intervals can be computed by the time series analysis method. The perturbations and fuel consumptions are addressed during the computation of the thrusters working time intervals. Next, the switching control law under constant thrust is designed for active collision avoidance maneuvres along a specified trajectory.At last, a monte carlo analysis is performed to calculate the relative velocities at which there are the possibility of collision. The simulation results show that with the switching control law, the chaser will maneuver along the specified trajectory and the goal of the collision avoidance can be achieved.

No associations

LandOfFree

Say what you really think

Search LandOfFree.com for scientists and scientific papers. Rate them and share your experience with other people.

Rating

Constant thrust collision avoidance maneuver under thruster failure 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 Constant thrust collision avoidance maneuver under thruster failure, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Constant thrust collision avoidance maneuver under thruster failure will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFWR-SCP-O-749798

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.