session 8

Title: Attitude Dynamics (1)
type: oral
Description: This theme discusses advances in spacecraft attitude dynamics and control, as well as design, testing and performance of novel attitude sensors and actuators. This theme also covers dynamics and control of multiple interconnected rigid and flexible bodies, including tethered systems, and in-orbit assembly.
Date: 2016-09-30
Time: 09:45
Room: Salon Jalisco E6

IPC members

Co-Chair: Dr. Hao-Chi Chang, tiSPACE Inc., Unknown;
Co-Chair: Prof. Gianmarco Radice, Singapore, Republic of;
Rapporteur: Dr. Shinji Hokamoto, Kyushu University, Japan;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		Inverse Dynamics Particle Swarm Optimization applied to constrained minimum-time maneuvers using reaction wheels	accepted	15'	confirmed	Mr. Dario Spiller	Sapienza University of Rome	Italy
2		Concept Design for a Satellite with Micro Vibration Isolator	accepted	15'	confirmed	Mr. Takuma Shibata	The Graduate Universty for Advanced Studies[SOKENDAI]	Japan
3		torque distribution algorithm for effective use of reaction wheels torque and angular momentum	accepted	15'	confirmed	Mr. Mikihiro Sugita	Mitsubishi Electric Corporation	Japan
4		Using Aerodynamic Torques to Aid Detumbling into an Aerostable State	accepted	15'	confirmed	Mr. Zhou Hao	The University of Manchester	United Kingdom
5		An attitude determination and control system for a nano-satellite alternative launch platform	accepted	15'	confirmed	Prof. Simone Battistini	Universidade de Brasília	Brazil
6		analysis and design of logical differential control law	accepted	15'	confirmed	Mr. XinXin Yu	Beijing Institute of Control Engineering(BICE), China Academy of Space Technology(CAST)	China
7		Stability Analysis of 3-axis Attitude Control System of Single Wing Satellite	accepted	15'	confirmed	Dr. Hao-Chi Chang	National Space Organization	Taiwan, China
8		Simple Adaptive Control of a Satellite with Large Flexible Appendages	accepted	15'	confirmed	Dr. Derek Gransden	Delft University of Technology (TU Delft)	The Netherlands
9		numerical evaluation of on-orbit attitude behavior for microsatellites with variable shape function	accepted	15'	confirmed	Mr. Kyosuke Tawara	Tokyo Institute of Technology	Japan
10		ACS Feed-Forward for Manipulator Control During Coupled Satellite Detumbling	accepted	15'	withdrawn	Mr. Barrett Dillow	University of Maryland, College Park	United States
11		Chaotic motions of tethered satellites with low thrust	accepted	15'	confirmed	Prof. Vladimir S. Aslanov	Samara National Research University (Samara University)	Russian Federation
12		Constraint Force Algorithm for Dynamics Modeling of Flexible Multibody Spacecraft	accepted	15'	confirmed	Ms. LI Haiyan		China
13		Dynamics and Underactuated Robust Control of Rigid-flexible Coupling Tethered System for Space Deorbit	accepted	15'	withdrawn	Dr. Liang Sun	Beihang University	China