Titlebook: Aerospace Mechatronics and Control Technology; Selected Contributio Huafeng Ding Conference proceedings 2022 The Editor(s) (if applicable)

Traumatic-Grief

Experimental Research on the Influence of the Bulk Swirl on the Compressorcompressor characteristic experiment under the overall vortex flow distortion generator based on the overall vortex flow distortion generator, and measured the performance of the swirl flow distortion generator. The generated swirl field obtains the pressure ratio and efficiency characteristics of t

混合物

Target Localization on Image-Guided Missilea target localization method that combines on-board IMU data and image information. This method does not require equipment such as GPS or optoelectronic platform, nor does it need prior knowledge or templates of the target. Firstly, a selection strategy is proposed to determine keyframes, which are

Leisureliness

Attitude Updating Algorithm Based on Agile Micro-Nano Satellites attitude updating algorithm of the traditional micro-nano satellite is no longer applicable. This paper proposes a modified attitude updating scheme applied to agile satellites. The method adopts the coning motion as the research scene, in which the influence of noncommutativity error is the worst.

lethal

歹徒

CANT

Simona Pekarek Doehler,Evelyne Berger flow around the blunt body with aerospike are investigated for the aerospike’s changing . ratios with freedom Mach number of 5.75. The effect of the characteristics of the flow field and the aerospike’s . ratios on the drag coefficient of model and the surface pressure coefficient of the nose cone

Latency

atrophy

https://doi.org/10.1007/978-3-030-22165-2t, the time domain and frequency domain identification should be carried out by measuring the performance indexes of the air rudder, which is used for the 6-DOF simulation of the aircraft. This paper designs the test platform and test scheme of the air rudder of the boost glide aircraft, and tests t

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gastritis

Simona Pekarek Doehler,Evelyne Bergercess, practical use, trial run, measurement and inspection by fishbone diagram. In order to ensure the economy and airworthiness of aero-engine manufacturing, the use and repair of bearing with skid damage were discussed by means of information statistics and trial run experiments. Then the effect o