Articles | Volume 11, issue 10
Atmos. Meas. Tech., 11, 5519–5530, 2018
https://doi.org/10.5194/amt-11-5519-2018
Atmos. Meas. Tech., 11, 5519–5530, 2018
https://doi.org/10.5194/amt-11-5519-2018

Research article 10 Oct 2018

Research article | 10 Oct 2018

Considerations for temperature sensor placement on rotary-wing unmanned aircraft systems

Brian R. Greene et al.

Download

Interactive discussion

Status: closed
Status: closed
AC: Author comment | RC: Referee comment | SC: Short comment | EC: Editor comment
Printer-friendly Version - Printer-friendly version Supplement - Supplement

Peer-review completion

AR: Author's response | RR: Referee report | ED: Editor decision
AR by Brian Greene on behalf of the Authors (25 Jul 2018)  Author's response    Manuscript
ED: Referee Nomination & Report Request started (30 Jul 2018) by Murray Hamilton
RR by Anonymous Referee #2 (25 Aug 2018)
ED: Publish subject to minor revisions (review by editor) (02 Sep 2018) by Murray Hamilton
AR by Brian Greene on behalf of the Authors (10 Sep 2018)  Author's response    Manuscript
ED: Publish as is (14 Sep 2018) by Murray Hamilton
Download
Short summary
With the recent commercial availability of rotary-wing unmanned aircraft systems (rwUAS), their ability to collect observations in the lower atmosphere is quickly being realized. However, integrating sensors with an rwUAS can introduce errors if not sited properly. This study discusses an objective method of determining some of these error sources in temperature, including improper airflow and rotary motor heating. Errors can be mitigated by mounting thermistors under propellers near the tips.