EXPLICIT FLATNESS-BASED GUIDANCE IN REENTRY PHASE

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ESMAELZADEH R.

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: Journal of Space Science and Technology Year:2014 | Volume:6 | Issue:4 (17) Page(s): 29-36

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Information Journal Paper

Title

EXPLICIT FLATNESS-BASED GUIDANCE IN REENTRY PHASE

Author(s)

ESMAELZADEH R. | Issue Writer Certificate

Keywords

REENTRYQ2

EXPLICIT GUIDANCEQ1

DIFFERENTIAL FLATNESSQ2

INVERSE DYNAMICSQ2

Abstract

An EXPLICIT GUIDANCE law is developed for a REENTRY vehicle. Motion is constrained to a three-dimensional Bezier curve. Acceleration commands are derived by solving an inverse problem that combined with DIFFERENTIAL FLATNESS approach. Trajectory is related to Bezier parameters. A comparison with pure proportional navigation shows the same accuracy, but a higher capability for optimal trajectory to some degree. Other advantages such as trajectory representation with minimum parameters, applicability to any REENTRY vehicle configuration and any control scheme, and Time-to-Go independency make this guidance approach more favorable.

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APA: Copy

ESMAELZADEH, R.. (2014). EXPLICIT FLATNESS-BASED GUIDANCE IN REENTRY PHASE. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 6(4 (17)), 29-36. SID. https://sid.ir/paper/150007/en

Vancouver: Copy

ESMAELZADEH R.. EXPLICIT FLATNESS-BASED GUIDANCE IN REENTRY PHASE. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2014;6(4 (17)):29-36. Available from: https://sid.ir/paper/150007/en

IEEE: Copy

R. ESMAELZADEH, “EXPLICIT FLATNESS-BASED GUIDANCE IN REENTRY PHASE,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 6, no. 4 (17), pp. 29–36, 2014, [Online]. Available: https://sid.ir/paper/150007/en

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