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61.
多个自由飞行空间机器人协调操作运动规划 总被引:2,自引:1,他引:2
本文提出了在空间微重力环境下多个自由飞行空间机器人协调操作运动规划算法,首先推导出多个自由飞行空间机器人协调操作的广义雅可比矩阵,其次给出了基于该矩阵的多个自由飞行空间机器人协调操作分解运动速度控制算法,最后用计算机仿真验证了该算法的正确性。 相似文献
62.
Features of fuel atomization and propagation in the flow behind a gas-dynamic stabilizer are considered. Estimations of the influence of transverse jets impulse magnitude on characteristics of mixing behind the stabilizer are obtained by numerical and experimental methods. 相似文献
63.
A technique of evaluating the micromechanical characteristics (namely, microhardness, microdurability, microbrittleness and
static crack resistance coefficient) using microindentation as applied to plasma zirconia-based thermal barrier coatings is
presented. 相似文献
64.
V. A. Mikheev S. D. Smol’nikov S. V. Surudin D. V. Savin 《Russian Aeronautics (Iz VUZ)》2016,59(1):145-150
The results of shaping process were obtained by the process scheme of serial stretching for biconvex skin of workpieces using the ANSYS/LS-DYNA software. The analysis is based on different flow material characteristics during plastic deformation at solid friction. A statistical analysis of the calculation results for disturbing factors assessment is carried out. 相似文献
65.
A. V. Bykov G. V. Kondrashev S. G. Parafes’ I. K. Turkin 《Russian Aeronautics (Iz VUZ)》2016,59(3):331-337
Theoretical and experimental methods of investigating the performance of an electric actuator of maneuverable unmanned aerial vehicle (UAV) is considered in order to solve the aeroelasticity tasks. Models of the stability analysis for the rudder–actuator system as well as the examples of numerical and experimental studies of this system performance are given. 相似文献
66.
The equations of the mathematical model are solved in terms of special functions. The results for the design scheme of the aircraft forebody are obtained with a guaranteed accuracy by the stable method of functional normalization. 相似文献
67.
We consider a probabilistic estimation of microaccelerations being produced in the inboard environment of an orbital laboratory as a random process; based on this estimation we analyzed a probability of fulfilling the favorable conditions to realize gravity-sensitive processes. The approach suggested can be applied when designing a space laboratory to meet the requirements for the microaccelerations inside the working zone of technological equipment. 相似文献
68.
S. A. Mikhailov L. V. Korotkov S. A. Alimov D. V. Nedel’ko 《Russian Aeronautics (Iz VUZ)》2011,54(3):247-253
A technique is suggested for calculating the helicopter spatial motion and the stress-strain state of a skid landing gear
in the course of landing with regard for the second landing impact; geometric, material and design nonlinearity of undercarriage
springs deformation is taken into account. The comparison between the analysis results and experimental data is presented. 相似文献
69.
70.
The investigation of stability and precision of the previously proposed implicit scheme of direct integration for the finite
element equations of motion is presented. The scheme parameter values that ensure its unconditional stability in the nonlinear
problems are determined and comparison with existing procedures is given. 相似文献