DocumentCode
1794649
Title
Longitudinal guidance and control of reentry vehicle in the approach and landing phase
Author
Chirayath, Bynu Benjamin ; Bindu, G.R.
Author_Institution
Coll. of Eng. Trivandrum, Thiruvananthapuram, India
fYear
2014
fDate
6-11 Jan. 2014
Firstpage
1
Lastpage
5
Abstract
Approach and Landing phase is an important and critical part of Reusable Launch Vehicle (RLV) mission. The challenging task is to deliver a RLV to its landing site safely and reliably. Hence a control scheme has to be designed that accomplishes this task. In this paper a well tuned PID controller was first designed. Using the inputs and outputs of the PID controller a Fuzzy logic controller was designed. The controller tracks the guidance commands and limits the angle of attack in order to steer the vehicle along the desired trajectory. Simulations were performed in MATLAB for the RLV using the above two controllers. The simulation results demonstrates that the latter controller offers better performance.
Keywords
aircraft landing guidance; control system synthesis; entry, descent and landing (spacecraft); fuzzy control; mathematics computing; space vehicles; three-term control; MATLAB; RLV mission; angle of attack; fuzzy logic controller; guidance commands; landing phase; reentry vehicle control; reentry vehicle longitudinal guidance; reusable launch vehicle mission; tuned PID controller; Acceleration; Aerodynamics; Fuzzy logic; Mathematical model; Trajectory; Vehicle dynamics; Vehicles; Approach and Landing; RLV; Reentry Fuzzy logic control;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Signals Control and Computations (EPSCICON), 2014 International Conference on
Conference_Location
Thrissur
Print_ISBN
978-1-4799-3611-3
Type
conf
DOI
10.1109/EPSCICON.2014.6887480
Filename
6887480
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