session 6

Title: Mission Design, Operations & Optimisation (1)
Description: The theme covers design, operations and optimisation of Earth-orbiting and interplanetary missions, with emphasis on studies and experiences related to current and future missions.
Date: 2013-09-26
Time: 09:45
Room: 306A

IPC members

Chairman: Prof. Michèle Lavagna, Politecnico di Milano, Italy;
Chairman: Prof. Kathleen Howell, Purdue University, United States;
Rapporteur: Prof. Igor V. Belokonov, Samara National Research University (Samara University), Russian Federation;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		ADR Mission Design and De-orbiting Strategies applied to Heavy Targets	accepted	15'	confirmed	Dr. Ciro Borriello	Aviospace S.R.L	Italy
2		Minimum-thrust problem and its application to trajectory optimization with thrust switchings	accepted	15'	confirmed	Dr. Viacheslav Petukhov	RIAME	Russian Federation
3		A Novel Nonlinear Guidance Scheme for Power-Limited Autonomous Rendezvous with Fixed Docking Direction and Collision Avoidance Constraints	accepted	15'	confirmed	Dr. Li Peng	Northwestern Polytechnical University	China
4		Optimal Low Thrust Deorbiting of Passively Stabilized LEO Satellites	accepted	15'	confirmed	Prof. Mikhail Ovchinnikov	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
5		Optimal low-thrust transfers in two-body and three-body dynamics	accepted	15'	confirmed	Mr. Mirco Rasotto	Politecnico di Milano	Italy
6		Optimization of operative planning and efficiency for multi-satellite observation and communication constellations	accepted	15'	confirmed	Dr. Valeriy V. Darnopykh	Moscow Aviation Institute (National Research University, MAI)	Russian Federation
7		novel numerical optimisation of the Hohmann Spiral Transfer	accepted	15'	confirmed	Mr. Steven Owens	Advanced Space Concept Laboratory, University of Strathclyde	United Kingdom
8		MULTIOBJECTIVE TRAJECTORY OPTIMIZATION OF SOLAR SAIL SPACECRAFT	accepted	15'	confirmed	Dr. Yang Zhang	Shanghai Institute of Satellite Engineering	China
9		Optimal law for inclination change in an atmosphere through solar sailing	accepted	15'	confirmed	Mr. Valentin Stolbunov	University of Toronto Institute for Aerospace Studies	Canada
10		High-Fidelity Optimum Electric Propulsion Transfer Design to GEO and MEO	accepted	15'	confirmed	Dr. Sven Erb	European Space Research and Technology Centre, ESA-ESTEC	The Netherlands
11		Optimal Lunar Landing Trajectory Design for Hybrid Engine	accepted	15'	confirmed	Dr. Dong-Hyun Cho	KARI	Korea, Republic of
12		Trajectory Optimization for Sun-Earth L5 Point Missions	accepted	15'	confirmed	Dr. Mingtao Li	National Space Science Center (NSSC), Chinese Academy of Sciences	China
13		A Study on Low-Cost and Flexible Deep Space Exploration Utilizing a Concept of Interplanetary Parking Orbit	accepted	15'	confirmed	Mr. Toshinori Ikenaga	Japan Aerospace Exploration Agency (JAXA)	Japan
14		New Technology for the Optimization of Low-Earth Orbit Satellite Maneuvers for the Purposes of Various Space Missions	accepted	15'	withdrawn	Mr. Alexander Moshnin	COSMOEXPORT Aerospace Research Agency	Russian Federation