Abstract
In this paper, leader-follower formation flying problems based on the periodic orbits of the Hill-Clohessy-Wiltshire equations and Tschauner-Hempel equations are considered. the control input is assumed to be impulsive. For a given final relative orbit, the admissible controls are feedback controls such that the follower tracks the final orbit asymptotically. The main performance index is the ΔV which is proportional to the fuel consumption. The number of impulses is fixed, but the impulse time is arbitrary and varied. The optimal location of impulse times is sought numerically. Simulation results for a reconfiguration problem are given.
| Original language | English |
|---|---|
| Title of host publication | 2nd IAA Conference on Dynamics and Control of Space Systems, 2014 |
| Publisher | Univelt Inc. |
| Pages | 861-872 |
| Number of pages | 12 |
| Volume | 153 |
| ISBN (Print) | 9780877036173 |
| Publication status | Published - 2015 |
| Event | 2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014 - Rome, Italy Duration: Mar 24 2014 → Mar 26 2014 |
Other
| Other | 2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014 |
|---|---|
| Country | Italy |
| City | Rome |
| Period | 3/24/14 → 3/26/14 |
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All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science
Cite this
Optimal selection of impulse times for formation flying. / Bando, Mai; Ichikawa, Akira.
2nd IAA Conference on Dynamics and Control of Space Systems, 2014. Vol. 153 Univelt Inc., 2015. p. 861-872.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
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TY - GEN
T1 - Optimal selection of impulse times for formation flying
AU - Bando, Mai
AU - Ichikawa, Akira
PY - 2015
Y1 - 2015
N2 - In this paper, leader-follower formation flying problems based on the periodic orbits of the Hill-Clohessy-Wiltshire equations and Tschauner-Hempel equations are considered. the control input is assumed to be impulsive. For a given final relative orbit, the admissible controls are feedback controls such that the follower tracks the final orbit asymptotically. The main performance index is the ΔV which is proportional to the fuel consumption. The number of impulses is fixed, but the impulse time is arbitrary and varied. The optimal location of impulse times is sought numerically. Simulation results for a reconfiguration problem are given.
AB - In this paper, leader-follower formation flying problems based on the periodic orbits of the Hill-Clohessy-Wiltshire equations and Tschauner-Hempel equations are considered. the control input is assumed to be impulsive. For a given final relative orbit, the admissible controls are feedback controls such that the follower tracks the final orbit asymptotically. The main performance index is the ΔV which is proportional to the fuel consumption. The number of impulses is fixed, but the impulse time is arbitrary and varied. The optimal location of impulse times is sought numerically. Simulation results for a reconfiguration problem are given.
UR - http://www.scopus.com/inward/record.url?scp=84968725193&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84968725193&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84968725193
SN - 9780877036173
VL - 153
SP - 861
EP - 872
BT - 2nd IAA Conference on Dynamics and Control of Space Systems, 2014
PB - Univelt Inc.
ER -