Solar sail transient dynamic analyzing method for determining effective propulsion acceleration breakage

A dynamic analysis and acceleration technology, applied in the field of transient dynamic analysis of solar sails, can solve the problems of large calculation error of the non-time-varying light pressure model, missing multiplication, and not considering the time-varying effect of light pressure.

Inactive Publication Date: 2015-04-01
CHINA ACADEMY OF SPACE TECHNOLOGY
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Problems solved by technology

[0004] However, solar sail researchers at home and abroad usually do not consider the time-varying effect of light pressure when calculating the transient effective propulsion acceleration
like figure 2 and image 3 As shown, the non-ideal plane of the initial state of the traditional solar sail surface and the two factors of the deformation of the sail surface during operation, the incident load of the time-invariant photopressure model is always perpendicular to the micro-element of the sail surface (thin solid line ), but the direction of the incident light ...

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  • Solar sail transient dynamic analyzing method for determining effective propulsion acceleration breakage
  • Solar sail transient dynamic analyzing method for determining effective propulsion acceleration breakage
  • Solar sail transient dynamic analyzing method for determining effective propulsion acceleration breakage

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Embodiment

[0067] Example: Static finite element simulation analysis of 160m solar sail structure

[0068] 1) Establish the finite element model of the solar sail, as shown in 4, which mainly includes: separately establish the support arm one-dimensional beam element and the sail surface two-dimensional triangular shell element model, set the square sail side length to 160m, and set the center body mass m center =100kg, end counterweight m vertex =12.4kg, the central body moment of inertia J center =0kg·m 2 , Support arm outer diameter D=300mm, wall thickness b=0.1mm, sail thickness h=1.5μm; set support arm material property E beam =210GPa, γ beam = 0.33, ρ beam =848kg / m 3 , Sail film material property E sail =2.5GPa, γ sail = 0.34, ρ sail =1420kg / m 3 ; Set the direction of prestress as two normal stresses in the sail surface, the magnitude is 50000Pa; Set the initial time t for solution 0 =0s, the final time t n = 400s and time step Δt = 0.5s, and the velocity and acceleration column...

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Abstract

The invention discloses a solar sail transient dynamic analyzing method for determining effective propulsion acceleration breakage. The solar sail transient dynamic analyzing method comprises the following steps: (1) establishing a solar sail finite element model; (2) entering the n-th solving moment and starting t from the t0+delta t; (3) calculating the rigidity matrix and the mass matrix of each sail area unit at the t moment under pre-stress according to the included angle of each sail area unit and the light pressure direction moment, thereby obtaining load of the area subjected to the light pressure of each sail area unit; (4) obtaining a global stiffness matrix Kt containing p units and the load row vector Ft as well as global mass m and the global mass matrix Mt; (5) calculating the final displacement, the final speed and the final acceleration of the t-th moment according to the final displacement, the final speed, the final acceleration at the (t-delta)-th moment, namely the initial conditions of the t-th moment as well as the global rigidity matrix and the load row vector at the t-th moment as well as the global mass matrix; (6) repeating steps (3)-(5) at the (t+delta t)-th moment until the final solving time tn; and (7) obtaining the breakage of the acceleration according to the results.

Description

Technical field [0001] The invention relates to a solar sail transient dynamics analysis method based on an accurate time-varying light pressure model for determining effective propulsion acceleration loss, and is especially suitable for various types of folds with unmeasured surface accuracy and different orbits and attitudes. The precise and effective acceleration analysis of the large super-flexible solar sail structure is determined. Background technique [0002] The solar sail is an advanced non-working medium long-term orbiting spacecraft. Because it only uses the reflected light pressure of the sun on a large area of ​​film to provide flight power, the solar sail spacecraft can continue to flow wherever there is sunlight. To gain power, eventually achieve speeds that ordinary spacecraft cannot reach. Because solar sails are not restricted by fuel and can run for a long time in the universe, they are especially suitable for deep space exploration missions. [0003] The sola...

Claims

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Application Information

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IPC IPC(8): G06F17/50
CPCY02E60/00
Inventor 杨辰刘宇飞张兴华王立侯欣宾
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
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