Parachute unfolding process stability assessment method of Mars parachute bag combination
A deployment process and parachute technology, applied in the aerospace field, can solve problems such as environmental and parameter uncertainty analysis, and achieve the effect of reducing the number of times and design costs, wide application range, and high repeatability
Active Publication Date: 2017-02-22
BEIJING INSTITUTE OF TECHNOLOGYGY
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Benefits of technology
This patented describes an improved way to evaluate how well a space shuttle's deploying mechanism works when it lands on another planet or other object during flight time. By doing this, researchers are able to better identify potential issues that may affect safety and performance of these spaceships.
Problems solved by technology
Technics Problem addressed in this patents are how to simplify the design of an improved space shuttle system used in lunar missions such as manned exploration or launches from Earth orbit towards outer planets with unknown environments and conditions that could affect its performance.
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Embodiment 1
[0121] A method for evaluating the stability of a parachute deployment process of a Mars umbrella cabin assembly disclosed in this embodiment comprises the following steps:
[0122] Step 1: Establish the umbrella cabin assembly model.
[0123] Step 1.1: Establish a reference coordinate system
[0124] (1) Return to the coordinate system o o x o the y o z o , abbreviated as O
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Abstract
The invention discloses a parachute unfolding process stability assessment method of a Mars parachute bag combination and relates to a parachute unfolding process stability assessment method and belongs to the technical field of aerospace. The parachute unfolding process stability assessment method adopts six-degree-of-freedom modeling, can conduct simulation analysis on center of mass motion in the parachute unfolding process and can also conduct simulation and assessment on parachute cabin gestures and the stress situations of hanging belts. Due to the fact that the established six-degree-of-freedommodel of the parachute cabin combination is simplified, the flow field analysis and flexible body modeling process can be omitted on the premise that it is ensured that simulationconforms to the actual physical situation, and the assessment and simulation efficiency is improved. The parachute unfolding process stability assessment precision and assessment efficiency of the Mars parachute bag combination can be improved, data support is provided for parachute and cabin parameter configuration, and the times and design costs of physical testing are reduced. In addition, the parachute unfolding process stability assessment method is feasible to different cabin type Mars landing tasks and is high in repeatability and wide in application range.
Description
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Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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