APAntonio Pedivellano
Antonio Pedivellano
*This is an algorithmically generated author record based on publicly available information.
Research Subjects
Research Interests
Antonio Pedivellano has a total of 4 co-authors. Here are the top co-authors by number of shared publications:
- Jaan Praks
Department of Electronics and Nanoengineering, Aalto University, Espoo, Finland
1 shared publication - Johannes Schumacher
Celestial Space Technologies GmbH, Nürnberg, Germany
1 shared publication - Mayank
Department of Electronics and Nanoengineering, Aalto University, Espoo, Finland
1 shared publication - Ville Lundén
Department of Electronics and Nanoengineering, Aalto University, Espoo, Finland
1 shared publication
Latest Publications
- Open Access
- 21 July 2025
- Published by Springer Nature in CEAS Space Journal
- Vol. 18 (5) , 1-11
Deployment and mounting system effects on a Ka-band reflectarray antenna: a sensitivity analysis
Reflectarray antennas are utilized in a wide variety of space missions as they combine benefits of reflector and phased array antennas. Large reflectarrays often require deployment mechanisms to enable their use on smaller satellites. The non-idealities of the reflector deployment system and the reflector mounting interfaces can significantly affect the radio frequency (RF) performance of the antenna. However, with lacking previous analysis on these effects, estimating the RF performance degradation is challenging, particularly at early design stages. This work aims to address this issue by analyzing the effects of mounting and deployment system non-idealities on a large, multipanel Ka-band (30 GHz) reflectarray antenna. The selected simulation analysis approach enables inducing and controlling small inaccuracies with high precision. This work shows that only $$0.10^{\circ }$$ and $$0.20^{\circ }$$ angular panel deployment inaccuracies lead to 1 dB and 3 dB gain loss, respectively. Typical reflector penetrating surface features can lead to more than 2 dB gain loss, and panel position inaccuracy out of the reflector plane starts rapidly degrading the gain performance after exceeding 1 mm. This work provides valuable data for estimating the magnitude of effects of non-ideal reflector mounting and deployment system features on large reflectarray antennas already at the start of the antenna design process.- 21 July 2025
- Published by Springer Nature in CEAS Space Journal
- Vol. 18 (5) , 1-11
Open AccessDeployment and mounting system effects on a Ka-band reflectarray antenna: a sensitivity analysis
Reflectarray antennas are utilized in a wide variety of space missions as they combine benefits of reflector and phased array antennas. Large reflectarrays often require deployment mechanisms to enable their use on smaller satellites. The non-idealities of the reflector deployment system and the reflector mounting interfaces can significantly affect the radio frequency (RF) performance of the antenna. However, with lacking previous analysis on these effects, estimating the RF performance degradation is challenging, particularly at early design stages. This work aims to address this issue by analyzing the effects of mounting and deployment system non-idealities on a large, multipanel Ka-band (30 GHz) reflectarray antenna. The selected simulation analysis approach enables inducing and controlling small inaccuracies with high precision. This work shows that only $$0.10^{\circ }$$ and $$0.20^{\circ }$$ angular panel deployment inaccuracies lead to 1 dB and 3 dB gain loss, respectively. Typical reflector penetrating surface features can lead to more than 2 dB gain loss, and panel position inaccuracy out of the reflector plane starts rapidly degrading the gain performance after exceeding 1 mm. This work provides valuable data for estimating the magnitude of effects of non-ideal reflector mounting and deployment system features on large reflectarray antennas already at the start of the antenna design process.