# Finite-time output feedback attitude control for spacecraft using “Adding a power integrator” technique

> Research article (Aerospace Science and Technology, 2017) · cited 77× · AI/ML

**Wikidata**: [openalex:W2601922245](https://www.wikidata.org/wiki/openalex:W2601922245)  
**Source**: https://4ort.xyz/entity/finite-time-output-feedback-attitude-control-for-spacecraft-using-adding-a-power-integrator-technique