Abstract The base of the dynamics characteristic research on the parachute and vehicle system is to establish a dynamics model, during the parachute descent phase, which can accurately display the relationship among the velocity, altitude and attitude angles as well as the variation of time. This paper starts with a new tracking law – ADRC in Mars entry guidance, which affects the initial states of the parachute deployment point and determines precision landing capability. Then, the influence of unsteady resistance to the parachute in Martian air is considered as the added mass, and a 6DOF nonlinear mathematical model of the parachute and vehicle system is established.
A 6DOF mathematical model of parachute in Mars EDL
Advances in Space Research ; 55 , 7 ; 1823-1831
2015-01-24
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
A 6DOF mathematical model of parachute in Mars EDL
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|Simulink Implementation of the 6DoF Model of Controlled Circular Parachute
British Library Conference Proceedings | 2002
|Mars Smart Lander Parachute Simulation Model
NTRS | 2002
|Mars Smart Lander Parachute Simulation Model
AIAA | 2002
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