Abstract
This paper investigates the cluster flight algorithm via the cyclic pursuit strategy in order to execute the coordination periodic motion of the distributed satellites. The proposed coordinated control law combining the cyclic pursuit strategy and diffeomorphism mapping is applied to match the trajectory of the cyclic pursuit and the natural periodic relative motion at low earth orbit environment considering the earth oblateness perturbation. The ultimate goal of the proposed method is to implement a cluster flight of multiple modules in the distributed satellite. Finally, a simulation example is presented to demonstrate the effectiveness of the proposed cluster flight algorithms.
Original language | English |
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Title of host publication | 2015 6th International Conference on Power Electronics Systems and Applications |
Subtitle of host publication | Electric Transportation - Automotive, Vessel and Aircraft, PESA 2015 |
Publisher | IEEE |
ISBN (Electronic) | 9781509000623 |
DOIs | |
Publication status | Published - 3 Feb 2016 |
Event | 6th International Conference on Power Electronics Systems and Applications, PESA 2015 - Hong Kong, Hong Kong Duration: 15 Dec 2015 → 17 Dec 2015 |
Conference
Conference | 6th International Conference on Power Electronics Systems and Applications, PESA 2015 |
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Country/Territory | Hong Kong |
City | Hong Kong |
Period | 15/12/15 → 17/12/15 |
Keywords
- cluster flight
- cyclic pursuit
- distributed satellite
- relative motion
ASJC Scopus subject areas
- Energy Engineering and Power Technology
- Control and Systems Engineering
- Electrical and Electronic Engineering