Vibration Reduction Using Command Generation in Formation Flying Satellites
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- Type
- dissertation
- Published
- 2005-04-18
- Cited by
- 6
- References
- 71
- Access
- Open access
- OpenAlex
- https://openalex.org/W40314094
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:108009069
Keywords
Reduction (mathematics), Vibration, Aerospace engineering, Satellite, Engineering
References
- MISSION ANALYSIS AND ORBIT CONTROL OF INTERFEROMETRIC WHEEL FORMATION FLYING
- Unity-Magnitude Input Shapers and their Relation to Time-Optimal Control
- Application of an adaptive control grid interpolation technique to morphological vascular reconstruction: a component of a comprehensive surgical planning and evaluation tool
- Formation flying mission for the UW Dawgstar satellite
- Closed-loop input shaping for flexible structures using time-delay control
- Advanced guidance algorithms for spacecraft formation-keeping
- EXTRA-INSENSITIVE INPUT SHAPERS FOR CONTROLLING FLEXIBLE SPACECRAFT
- Adaptive neural control of deep-space formation flying
- Creating emergent behaviors: two robotics labs that combine reactive behaviors
- Convolved and simultaneous two-mode input shapers
- Slewing Flexible Spacecraft with Deflection-Limiting Input shaping
- Formation Flying Control in Eccentric Orbits
- Time-Optimal Negative Input Shapers
- Preshaping Command Inputs to Reduce System Vibration
- Residual Vibration Reduction Using Vector Diagrams to Generate Shaped Inputs
- Study of Interspacecraft Coulomb Forces and Implications for Formation Flying
- Hybrid Cartesian and Orbit Element Feedback Law for Formation Flying Spacecraft
- Feedback Control for Slew Maneuver Using On -Off Thrusters
- Vibration Reduction for Flexible Spacecraft Following Momentum Dumping With/Without Slewing
- Robust Time-Optimal Control of Uncertain Flexible Spacecraft
Cited by
- Designing unity magnitude input shaping by using PWM technique
- Vibration suppression of a 3-PRR flexible parallel manipulator using input shaping
- Input shaping for control of satellites and formation of satellites
- Spacecraft Formation Flying Control
- Research on actuator effort and energy consumption of a parallel manipulator based on input shaping combined with PD
- DARBE GENİŞLİK MODÜLASYONU İLE SÜRÜLEN SİSTEMLERE GİRDİ ŞEKİLLENDİRME TEKNİĞİNİN UYGULANABİLİRLİĞİ
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