Abstract
In order to achieve mission success with more demanding mission requirements and more complex onboard software, our software independent verification and validation (IV&V) has been applied to various spacecraft software programs, such as software on satellites, ground stations, and the Japanese Experimental Module (JEM) of the International Space Station (ISS). The malfunction procedure in the operations data file for JEM is also the target for applying software IV&V. Suitable software IV&V can be performed for each spacecraft throughout the entire development life cycle. The objectives for software IV&V activity are the following: applying suitable software IV&V to each spacecraft, creating new software IV&V technologies for spacecraft, and spreading new software engineering technologies based on our software IV&V to development teams and contractors. This paper introduces our software IV&V activities and several examples to confirm that our activities are effective and efficient for spacecraft.
| Original language | English |
|---|---|
| Title of host publication | IEEE Aerospace Conference Proceedings |
| DOIs | |
| Publication status | Published - 2008 |
| Externally published | Yes |
| Event | 2008 IEEE Aerospace Conference, AC - Big Sky, MT, United States Duration: 2008 Mar 1 → 2008 Mar 8 |
Other
| Other | 2008 IEEE Aerospace Conference, AC |
|---|---|
| Country | United States |
| City | Big Sky, MT |
| Period | 08/3/1 → 08/3/8 |
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ASJC Scopus subject areas
- Aerospace Engineering
Cite this
Software independent verification and validation for spacecraft at JAXA. / Kohtake, Naohiko; Katoh, Atsushi; Ishihama, Naoki; Miyamoto, Yuko; Kawasaki, Tomomi; Katahira, Masafumi.
IEEE Aerospace Conference Proceedings. 2008. 4526598.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Software independent verification and validation for spacecraft at JAXA
AU - Kohtake, Naohiko
AU - Katoh, Atsushi
AU - Ishihama, Naoki
AU - Miyamoto, Yuko
AU - Kawasaki, Tomomi
AU - Katahira, Masafumi
PY - 2008
Y1 - 2008
N2 - In order to achieve mission success with more demanding mission requirements and more complex onboard software, our software independent verification and validation (IV&V) has been applied to various spacecraft software programs, such as software on satellites, ground stations, and the Japanese Experimental Module (JEM) of the International Space Station (ISS). The malfunction procedure in the operations data file for JEM is also the target for applying software IV&V. Suitable software IV&V can be performed for each spacecraft throughout the entire development life cycle. The objectives for software IV&V activity are the following: applying suitable software IV&V to each spacecraft, creating new software IV&V technologies for spacecraft, and spreading new software engineering technologies based on our software IV&V to development teams and contractors. This paper introduces our software IV&V activities and several examples to confirm that our activities are effective and efficient for spacecraft.
AB - In order to achieve mission success with more demanding mission requirements and more complex onboard software, our software independent verification and validation (IV&V) has been applied to various spacecraft software programs, such as software on satellites, ground stations, and the Japanese Experimental Module (JEM) of the International Space Station (ISS). The malfunction procedure in the operations data file for JEM is also the target for applying software IV&V. Suitable software IV&V can be performed for each spacecraft throughout the entire development life cycle. The objectives for software IV&V activity are the following: applying suitable software IV&V to each spacecraft, creating new software IV&V technologies for spacecraft, and spreading new software engineering technologies based on our software IV&V to development teams and contractors. This paper introduces our software IV&V activities and several examples to confirm that our activities are effective and efficient for spacecraft.
UR - http://www.scopus.com/inward/record.url?scp=49349113300&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=49349113300&partnerID=8YFLogxK
U2 - 10.1109/AERO.2008.4526598
DO - 10.1109/AERO.2008.4526598
M3 - Conference contribution
AN - SCOPUS:49349113300
SN - 1424414881
SN - 9781424414888
BT - IEEE Aerospace Conference Proceedings
ER -