• Home
  • Current congress
  • Public Website
  • My papers
  • root
  • browse
  • IAC-15
  • C1
  • session IP
  • IP. Interactive Presentations

    Papers

    2. an improved shape-based method using fourier series for low-thrust orbit design

    3. Guide star catalog for satellite attitude estimation

    4. DYNAMICS OF ORBITS FOR SPACE MISSIONS TAKING INTO ACCOUNT A DISTURBING BODY IN AN ELLIPTICAL-INCLINATED ORBIT: APPLICATIONS TO PLANETARY MOONS

    5. Shorter rotation path design in under-actuated wheel spacecraft

    6. Modeling and direct adaptive control of a manipulator with variable-speed control moment gyroscopes

    7. Study on the system of a novel space borne ultra-quiet platform of double drag-free based on the electrostatic levitation

    8. A Ground Attitude Analysis Method of the LEO Satellite employing large-scale Rotating Instruments

    9. Constraints Handling Method in Indirect Trajectory Optimization for Manned Asteroid Exploration

    11. Implementation, Tests and Characterization Results for CubeSat ADCS

    12. A NOVEL ATTITUDE QUATERNION FILTER FOR THE ESA EUROPEAN STUDENT EARTH ORBITER (ESEO)

    13. Attitude stabilization controller for underatuated spacecrafts based on hierarchical adaptive sliding-mode control

    14. Useful alternative parameterization of an orbital state vector with application to formations of LEO satellites

    15. A MONOCULAR-BASED RELATIVE POSITION AND ATTITUDE FILTERING FOR UNKNOWN TARGETS

    16. Analytic parametrisation of periodic orbits around the rotational equilibria of an asteroid perturbed by Sun gravity and radiation pressure

    17. Relative orbital motion analysis using dual Lie algebra representations

    18. PANGU-4 Simulation Tool for the Testing of Vision-Based Navigation for Planetary Landers

    19. robust control and double flexible vibration active suppression of space robot with flexible-link and flexible-joint that used in space station

    20. The Homoclinic and Heteroclinic Connections of Planar Symmetric Resonant Orbits in the Restricted Three-Body Earth-Moon System

    21. Compact Finite-Difference Method for Planetary Flyby Orbit Design