session 9
- Title
Guidance, Navigation and Control - Part 3
- type
oral
- Description
The emphasis of this theme is on the studies and application related to the guidance, navigation and control of earth-orbiting and interplanetary spacecraft and rockets, including rendezvous and docking.
- Date
2011-10-07
- Time
- Room
- IPC members
Chairman: Prof. Weihua Zhang, National University of Defense Technology, China;
Chairman: Prof. Saburo Matunaga, Tokyo Institute of Technology, Japan;
Rapporteur: Dr. Bernard Lübke-Ossenbeck, OHB System AG-Bremen, Germany;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | Guidance, Navigation, and Control System Design of HTV and Evaluation of On-orbit Results | 15 | confirmed | Dr. Shoji Yoshikawa | Mitsubishi Electric Corporation | Japan | |
2 | Rendezvous Technique of HTV and Evaluation of On-orbit Results | 15 | confirmed | Dr. Shoji Yoshikawa | Mitsubishi Electric Corporation | Japan | |
3 | An On-Orbit Mass Properties Identification Algorithm for Large Space Structures | 15 | confirmed | Ms. Ling Jiang | Beihang University | China | |
4 | Spacecraft Actuator Alignment Determination through Null Motion Excitation | 15 | confirmed | Dr. Frederick Leve | Air Force Research Laboratory (AFRL) | United States | |
5 | Global and local optimization approaches for launch vehicles ascent trajectory design | 15 | confirmed | Ms. Annalisa Riccardi | University of Bremen | Germany | |
6 | 15 | no-show | Dr. Nie Qi | Beijing Aerospace Automatic Control Institute | China | ||
7 | 15 | confirmed | Mr. Steven Owens | Advanced Space Concept Laboratory, University of Strathclyde | United Kingdom | ||
8 | Mathematical model for attitude control of small satellites using rotation angles | 15 | confirmed | Prof. Teodor-Viorel Chelaru | University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space | Romania | |
9 | In-Orbit Identification of Moment of Inertia Matrix for High Pointing Satellites | 15 | confirmed | Mr. Bharadwaj K.M. | Indian Space Research Organization (ISRO) | India | |
10 | Neural Network Based Predictor-Corrector Entry Guidance for High Lifting Vehicles | 15 | withdrawn | Mr. Mingliang Xu | National University of Defense Technology | China | |
11 | Derivation of a Complete Set of Equations of Motion for Coupled Slosh-Vehicle Dynamics | 15 | confirmed | Dr. Mohammad Ebrahimi | Aerospace Research Institute | Iran |