The Basis HALO Measurement and Sensor System (BAHAMAS)
PMS probes in under-wing carriers over the Alps
credit: DLR
HALO with air inlets on top
credit: DLR-FX
Cabin with LIDAR instruments installed
photo taken during NAWDIC | credit: A. Minikin (DLR-FX)
Instrument integration test
credit: DLR-FX
HALO noseboom from the cockpit
photo taken during ACRIDICON-CHUVA | credit: M. Heckl (U. Leipzig)
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Description
HALO is equipped with a basis sensor system permanently installed at the aircraft, called BAHAMAS (Basic Halo Measurement and Sensor System). BAHAMAS was developed by the Instrumentation and Data Science Group of the Flight Experiments Facility of DLR and supports the science projects on HALO with a basic data set which describes the aircraft state and air data for the surrounding atmosphere.
BAHAMAS consists of several components:
- A main data acquisition rack in the rear cabin
- An instrumented box in the unpressurized nose section
- 6 Total Air Temperature (TAT) inlets in the aircraft nose section
- An instrumented nose boom
- GPS antennas, a data distribution network, …..
Concerning the aircraft state parameters, the system directly monitors several avionic systems of the Gulfstream G550 (Air Data System, Flight Management HALO Airflow Sensor Calibration Computer, Inertial Reference System etc. via ARIC 429) as well as the main aircraft avionic bus ASCB-D.
For the measurement of pressure, temperature, humidity and wind vector
BAHAMAS deploys a set of own sensors:
- An experimental Inertial Reference System (IRS)
- Temperature sensors in selected TAT housings
- Humidity sensors in the nose box and in the main data acquisition rack
- An airflow sensor with pitot static probe at the tip of the nose boom
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Data
The BAHAMAS datastream contains all basic information needed to evaluate and reference measurements taken with the equipment installed on HALO during a mission. Moreover, BAHAMAS provides precise measurements of various atmospheric parameters, which are used for scientific evaluation in itself.
BAHAMAS data includes:
- Access to the basic aircraft position data
- Measurement of the 3-D wind field and turbulence
- Measurement of pressure and temperature
- Measurement of humidity with different seonsors up to the tropopause level
- Radiation
- Surrounding conditions in the aircraft
- Aircraft Parameter from the Air Data Computer
- Video Signals
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References
Giez, Andreas und Mallaun, Christian und Nenakhov, Vladyslav und Zöger, Martin (2025): Calibration of a Nose Boom Mounted Airflow Sensor on an Atmospheric Research Aircraft by Inflight Maneuvers. DLR-Forschungsbericht. DLR-FB-2025-17. 195S. doi: 10.57676/7wf2-dk78.
Giez, Andreas und Zöger, Martin und Mallaun, Christian und Nenakhov, Vladyslav und Schimpf, Marina und Grad, Christoph und Numberger, Andreas und Raynor, Kevin (2023): Determination of the Measurement Errors for the HALO Basic Data System BAHAMAS by Means of Error Propagation. DLR-Forschungsbericht. DLR-FB-2022-27. 97S. doi: 10.57676/5rdc-q708.
Giez, Andreas und Mallaun, Christian und Nenakhov, Vladyslav und Zöger, Martin (2021): Calibration of a Nose Boom Mounted Airflow Sensor on an Atmospheric Research Aircraft by Inflight Maneuvers. DLR-Forschungsbericht. DLR-FB-2021-17. 179S.
Giez, Andreas und Zöger, Martin und Dreiling, Volker und Mallaun, Christian (2020): Static Source Error Calibration of a Nose Boom Mounted Air Data System on an Atmospheric Research Aircraft Using the Trailing Cone Method. DLR-Forschungsbericht. DLR-FB-2019-7. Deutsches Zentrum für Luft- und Raumfahrt. 87S.
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User instrumentation
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Special structures for HALO instrumentation
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