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830 results for “Attitudes”
GO JUPTER POS ANCILLARY ROTOR ATTITUDE V1.0
This data set contains the attitude data for the rotor of the Galileo spacecraft. The data provided are derived from the Attitude and Articulation Control System (AACS) data downlink as provided by the Galileo project to the magnetometer team. This data set covers portions of the Jupiter Approach (JA) and all orbit operation mission phases (J0-J35). The data are discontinuous. The sampling frequency varies with mission phase. The coverage period is from 1995-11-28T01:34 to 2001-09-21 (exact time of last sample is currently unknown).
Wind Definitive Attitude, 10 min Data, Spin Axis Orientation Angles in GCI, GSE and GSM Coordinates
Wind Definitive Attitude Body Spin Rate and Spin Axis Orientation Right Ascension and Declination Angles in Geocentric Celestial Inertial, GCI, Geocentric Solar Ecliptic, GSE, and Geocentric Solar Magnetospheric, GSE, Coordinates
LP MOON SPACECRAFT ATTITUDE V1.0
The Lunar Prospector attitude data set consists of values for the spacecraft spin rate and spin axis orientation (attitude) as a function of time. These values are determined from spacecraft attitude data (sun and limb crossing sensors) and ephemeris data. Spacecraft orientations are given as right ascension and declination of the spacecraft spin axis in the Mean-of-J2000 Ecliptic reference frame. The attitude data set consists of a single, cumulative file for the entire mission. Records are added to this file following each significant change in either the spin rate or spin axis orientation. The spacecraft spin rates and attitudes in this data set are orbit averages. The instantaneous spin rate can be determined from the sun pulse data set. The instantaneous spin rate varies as the spacecraft passes into and out of the Moon's shadow and after each spacecraft maneuver. Generally, an attitude record is included for times immediately before and after each maneuver.
Wind Predicted Attitude, 10 min Data, Spin Axis Orientation Angles in GCI, GSE and GSM Coordinates
Wind Predicted Attitude Body Spin Rate and Spin Axis Orientation Right Ascension and Declination Angles in Geocentric Celestial Inertial, GCI, Geocentric Solar Ecliptic, GSE, and Geocentric Solar Magnetospheric, GSE, Coordinates
Ground-Based Global Navigation Satellite System (GNSS) Galileo real-time POD Attitude Quaternions (30-second sampling, 60-second files) from NASA CDDIS
This product contains a time series of attitude quaternion components for healthy satellites in the Galileo constellation that are accumulated every minute throughout the day. The product is generated at JPL's Global Differential GPS Operations Centers in real-time. The data in this product can be concatenated with other daily products to provide larger coverage in time.
TWINS-2 Ephemeris, Definitive Spacecraft Attitude, PT0.512S Data
Two Wide-angle Imaging Neutral-atom Spectrometers 2, TWINS 2, Spacecraft Attitude data, Earth Centered Inertial, ECI, coordinates. This TWINS data set contains spacecraft attitude data as polar and azimuthal instrument pointing vectors. The polar vector points along the TWINS rotation axis. The azimuthal vector lies in the plane normal to the polar vector and points toward the central scanning position, which is defined as the zero-point location. Such pointing is derived from both the spacecraft attitude history, SAH, file and the sensor mounting orientation. The computation employed is designed to achieve a pointing accuracy of 0.5°. Any deviation from this accuracy level is indicated in the header record metadata.
ROSETTA ATTITUDE & ORBIT CONTROL SYSTEM ENGINEERING DATA
This CODMAC level 3 data set contains the key parameters of the AOCMS. In particular, it provides information on the Attitude & Orbit Control Management System operating modes as well as Wheel offloading data. It covers the period from launch in 2004, through the 3 Earth and 1 Mars flyby, plus the hibernation phases, plus the asteroid flybys and finally covers the Prelanding, comet escort & Extension phases of the prime target of the mission. The prime target is comet 67P/Churyumov-Gerasimenko 1 (1969 R1). This version V1.0 is the first version of this dataset.
Ground-Based Global Navigation Satellite System (GNSS) GPS real-time POD Attitude Quaternions (30-second sampling, 60-second files) from NASA CDDIS
This product contains a time series of attitude quaternion components for healthy satellites in the GPS constellation that are accumulated every minute throughout the day. The product is generated at JPL's Global Differential GPS Operations Centers in real-time. The data in this product can be concatenated with other daily products to provide larger coverage in time.
ECOSTRESS Attitude Daily L1B Global 70m V001
The ECOsystem Spaceborne Thermal Radiometer Experiment on Space Station (ECOSTRESS) mission measures the temperature of plants to better understand how much water plants need and how they respond to stress. ECOSTRESS is attached to the International Space Station (ISS) and collects data globally between 52 degrees N and 52 degrees S latitudes. A map of the acquisition coverage can be found in figure 2 on the ECOSTRESS website (https://ecostress.jpl.nasa.gov/science). The ECO1BATT Version 1 data product provides both corrected and uncorrected attitude quaternions and spacecraft ephemeris data obtained from the ISS. The data are provided in 1 second intervals by the ISS, and each product file contains vectors from the duration of the orbit. The time elements are copied from the ISS raw data. The ECO1BATT Version 1 data product contains variables of corrected and uncorrected attitude quaternions, spacecraft ephemeris data including Earth-centered inertial (ECI) position and velocity, and associated time elements. Known Issues * Cannot perform spatial query on ECO1BATT in NASA Earthdata Search: ECO1BATT does not contain spatial attributes, so granules cannot be searched by geographic location. Users should search for ECO1BATT data products by orbit number instead. * Data acquisition gap: ECOSTRESS was launched on June 29, 2018, and moved to autonomous science operations on August 20, 2018, following a successful in-orbit checkout period. On September 29, 2018, ECOSTRESS experienced an anomaly with its primary mass storage unit (MSU). ECOSTRESS has a primary and secondary MSU (A and B). On December 5, 2018, the instrument was switched to the secondary MSU and science operations resumed. On March 14, 2019, the secondary MSU experienced a similar anomaly temporarily halting science acquisitions. On May 15, 2019, a new data acquisition approach was implemented and science acquisitions resumed. To optimize the new acquisition approach TIR bands 2, 4 and 5 are being downloaded. The data products are as previously, except the bands not downloaded contain fill values (L1 radiance and L2 emissivity). This approach was implemented from May 15, 2019, through April 28, 2023. * Data acquisition gap: From February 8 to February 16, 2020, an ECOSTRESS instrument issue resulted in a data anomaly that created striping in band 4 (10.5 micron). These data products have been reprocessed and are available for download. No ECOSTRESS data were acquired on February 17, 2020, due to the instrument being in SAFEHOLD. Data acquired following the anomaly have not been affected. * Data acquisition: ECOSTRESS has now successfully returned to 5-band mode after being in 3-band mode since 2019. This feature was successfully enabled following a Data Processing Unit firmware update (version 4.1) to the payload on April 28, 2023. To better balance contiguous science data scene variables, 3-band collection is currently being interleaved with 5-band acquisitions over the orbital day/night periods.
Polar Definitive Attitude, 10 min Data, Spin Axis Orientation Angles in GCI, GSE and GSM Coordinates
Polar Definitive Attitude Body Spin Rate and Spin Axis Orientation Right Ascension and Declination Angles in Geocentric Celestial Inertial, GCI, Geocentric Solar Ecliptic, GSE, and Geocentric Solar Magnetospheric, GSE, Coordinates
Attitude Scenario Data PVact Exploration
<p>This data comprises the files for the attitude-varying scenarios in the PVact exploration paper.</p> <p>The .csv and .xls files comprise the data of the respective (sub-)scenarios, whereas the .sh scripts document how the data was downloaded. The calculations were done on the infrastructure of the Leipzig Computing Center as is documented in the respective paper. </p>
Entrepreneurial intention from the attitude and behavioral control of university students
<p><strong><span>Abstract: </span></strong><span>This study examines the influence of attitude and perceived behavioral control on the entrepreneurial intentions of university students in Ayacucho, Peru. Utilizing structural equation modeling (SEM) and data from 468 students, the research validated its findings through exploratory and confirmatory factor analyses. The results indicate that both attitude and perceived behavioral control are significant predictors of entrepreneurial intention, together explaining 37% of its variance. Attitude emerged as the most influential factor, accounting for 33%, while perceived behavioral control contributed 19%. These findings support the Theory of Planned Behavior (TPB) and highlight the necessity of educational strategies that promote both constructs to enhance entrepreneurial intent among students. This study offers valuable insights for higher education, suggesting that programs should not only focus on technical skills but also cultivate positive attitudes and a sense of control over entrepreneurial processes. Given that entrepreneurship is crucial for regional economic development, the implications extend to informing educational policies and initiatives aimed at fostering youth entrepreneurship. Furthermore, unlike prior research that typically treated attitude and perceived behavioral control separately, this study integrates both constructs within a comprehensive TPB and Self-Determination Theory framework, reinforcing their combined effect on entrepreneurial intentions.</span></p> <p> </p>
Attitudes to predation by domestic cats differs between conservation researchers and conservation practitioners, and are influenced by cat ownership
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Attitudes towards mandatory vaccination and the COVID certificate as a function of vaccination status and risk perception: A vignette-based study
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An Exploratory Comparison of Attitudes Toward Stuttering and Cluttering of Chinese Practicing Speech and Language Therapists (SLTs) and SLT Students
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Assessment of fear of death and attitudes toward dying patients in nursing students during their academic training
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Gardening for biodiversity: an empirical exploration of garden owner's barriers, attitudes, and gardening behaviors - DATASET
<p>Correspondance author: Oriol García-Antúnez. University of Copenhagen, Department of Geosciences and Natural Resource Management, Rolighedsvej 23, 1958 Frederiksberg C, Denmark. e-mail: oga@ign.ku.dk</p> <p> </p>
Data of Implicit and Explicit Test of Consumer Attitudes to Organic Food Attributes: Case of Lithuanian Consumers
<p>The implicit and explicit test of consumer attitudes to organic food attributes includes responses from 302 research participants from Lithuania. Fourteen organic food attributes were included in the research. Additionally, the data set provides demographic data of the research participants. The data was collected in the fourth quarter of 2021.</p>
RESULTS - attitudes towards household waste separation in Slovenia
<p><strong>Attitudes towards household waste separation in Slovenia (in 2020)</strong></p> <p>In the subsequent phase of our research, we centred our attention on consumers to gain insights into their understanding and feelings about separating packaging waste. Utilizing an online questionnaire named 'Waste packaging' as our primary data collection tool, we segmented the questionnaire into three main sections: respondents' socio-economic background, their personal pro-environmental behaviours and external factors such as current waste collection systems. We aimed to capture a comprehensive sample of adult Slovenian citizens, reaching out via email, social media and community channels.</p>
Polar Electric Fields Instrument (EFI), Spacecraft Attitude in GSE coordinates
the Polar spacecraft positive spin axis direction vector (normalized to magnitude 1), in GSE coordinates.
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