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2020, 05, No.203 52-65
Development Analysis of Guidance Technology for Aerospace Vehicle Based on Combination Engine
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DOI: 10.16358/j.issn.1009-1300.2020.1.088
Abstract:

The flight mission characteristics of aerospace vehicle based on combination engine have put forward high requirements for guidance technology. Starting from the flight profile of aerospace vehicle,the research status of guidance technology related to the combination power climbing phase,rocket power orbital phase,reentry phase,energy management phase and autonomous landing phase are introduced.On this basis,the key guidance problems that need to be further solved to meet the mission capability improvement for aerospace vehicle based on combination engine are analyzed. And then this paper can provide a certain reference for developing the future research direction of guidance technology for aerospace vehicle.

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Basic Information:

DOI:10.16358/j.issn.1009-1300.2020.1.088

China Classification Code:V448.2;V249

Citation Information:

[1]She Wenxue,Liu Kai,Qiao Hong ,et al.Development Analysis of Guidance Technology for Aerospace Vehicle Based on Combination Engine[J].Tactical Missile Technology,2020,No.203(05):52-65.DOI:10.16358/j.issn.1009-1300.2020.1.088.

Published:  

2020-09-15

Publication Date:  

2020-09-15

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