J. T. Halbert
Papers
1
Total Citations
32
H-Index
1
About
J. T. Halbert is a researcher specializing in spacecraft attitude determination and control, with a particular focus on low-cost sensor integration. His most-cited work, "Rigid body attitude control with inclinometer and low-cost gyro measurements" (2003, 32 citations), addresses a critical challenge in small satellite missions: achieving reliable attitude estimation using affordable, off-the-shelf sensors. By combining inclinometer data with low-cost gyroscopes, Halbert demonstrated a practical method for maintaining rigid body orientation without expensive inertial measurement units, making precision attitude control more accessible for educational and resource-constrained space projects. This contribution has influenced subsequent work in sensor fusion and fault-tolerant control systems. While his citation count reflects a focused niche, Halbert’s research underscores the importance of cost-effective solutions in expanding space technology access. His work remains relevant for engineers developing CubeSats and microsatellites, where budget limitations demand innovative approaches to traditional control problems.
Research Focus
Key Achievements
Top Papers
- 1Rigid body attitude control with inclinometer and low-cost gyro measurements32 citations · 2003