Discrete flight path angle tracking control of hypersonic flight vehicles via multi-rate sampling
This paper presents the flight path angle tracking control of the longitudinal dynamics of a generic hypersonic flight vehicle(HFV). Due to the use of digital computers and microprocessors for controls applications, the discrete hypersonic flight control is investigated. The altitude command is tran...
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Main Authors: | , , , , |
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Other Authors: | |
Format: | Conference or Workshop Item |
Language: | English |
Published: |
2013
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Online Access: | https://hdl.handle.net/10356/98868 http://hdl.handle.net/10220/12652 |
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Institution: | Nanyang Technological University |
Language: | English |