Three-Axis Satellite Attitude Control Based on Magnetic Torquing: Linear Optimal Approach

Research output: Contribution to book/anthology/report/conference proceedingArticle in proceedingResearch

Abstract

Recently small satellite missions have gained considerable interest due to low-cost launch opportunities and technilogical improvement of micro-electronics.
Original languageDanish
Title of host publication10th IFAC Workshop on Control Applications of Optimization
Publication date1995
Publication statusPublished - 1995
EventThree-Axis Satellite Attitude Control Based on Magnetic Torquing -
Duration: 19 May 2010 → …

Conference

ConferenceThree-Axis Satellite Attitude Control Based on Magnetic Torquing
Period19/05/2010 → …

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