Abstract
This paper presents the identification of inertia parameters, such as mass, moment of inertia and the product of inertia, for a free-flying space robot. Making use of the conservation of momentum, an identification algorithm that does not require torque or acceleration measurement is developed. Gravity gradient torques are also used to identify the product of inertia. The algorithm is verified with the flight data obtained by the ETS-VII, Japanese space robot.
| Original language | English |
|---|---|
| Title of host publication | AIAA Guidance, Navigation, and Control Conference and Exhibit |
| Publisher | American Institute of Aeronautics and Astronautics Inc. |
| ISBN (Print) | 9781563479786, 9781624101083 |
| DOIs | |
| Publication status | Published - 2002 |
| Externally published | Yes |
| Event | AIAA Guidance, Navigation, and Control Conference and Exhibit 2002 - Monterey, CA, United States Duration: 2002 Aug 5 → 2002 Aug 8 |
Publication series
| Name | AIAA Guidance, Navigation, and Control Conference and Exhibit |
|---|
Conference
| Conference | AIAA Guidance, Navigation, and Control Conference and Exhibit 2002 |
|---|---|
| Country | United States |
| City | Monterey, CA |
| Period | 02/8/5 → 02/8/8 |
ASJC Scopus subject areas
- Aerospace Engineering
- Control and Systems Engineering
- Electrical and Electronic Engineering
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Cite this
Yoshida, K., & Abiko, S. (2002). Inertia parameter identification for a free-flying space robot. In AIAA Guidance, Navigation, and Control Conference and Exhibit (AIAA Guidance, Navigation, and Control Conference and Exhibit). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2002-4568