AEROSPACE SHANGHAI, Volume. 41, Issue 4, 1(2024)
Fixed Time Control of RLV landing Section Under the Influence of Complex Wind Field
Fig. 1. Change curve of the additional angle of attack under the downwind condition
Fig. 2. Change curve of the additional side slip angle under the downwind condition
Fig. 3. Change curve of the additional angle of attack under the headwind condition
Fig. 4. Change curve of the additional angle of attack under the headwind condition
Fig. 6. Change curves of the attitude angle under different conditions
Fig. 7. Change curves of the attitude angular velocity under different conditions
Fig. 8. Change curves of the attitude angle under different control laws
Fig. 9. Change curves of the attitude angle rate under different control laws
Fig. 10. Change curves of the disturbance observation values and the observation errors
Fig. 11. Change curves of the control moments under different control laws
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Naigang CUI, Guoxin QU, Yuhao ZHANG. Fixed Time Control of RLV landing Section Under the Influence of Complex Wind Field[J]. AEROSPACE SHANGHAI, 2024, 41(4): 1
Category: Special Paper of Expert
Received: Jun. 25, 2024
Accepted: --
Published Online: Nov. 18, 2024
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