Abstract
The Take-Off Performance Monitor (TOPM) reviewed in this paper has the capacity to detect and declare performance deficiencies during the ground roll by considering critical take-off lengths, current achieved acceleration and engine health. The Mass Momentum Method (MMM) and the Simplified Gross Thrust Method (SGTM) are proposed as suitable methods to compute in-flight gross thrust.
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References
Hughes, D.L. (1981) Comparison of Three Thrust Calculation Methods Using In-Flight Thrust Data, NASA TM-81360.
Khatwa, R. (1990) The Development of a Take-Off Performance Monitor, PhD Thesis (in preparation), University of Bristol.
Srivatsan, R. et al. (1987) Development of a takeoff performance monitoring system, J. Guidance and Control, 10, 433–440.
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© 1990 Chapman and Hall
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Khatwa, R. (1990). Engine monitors for efficient take-Off performance monitors. In: Rao, R.B.K.N., Au, J., Griffiths, B. (eds) Condition Monitoring and Diagnostic Engineering Management. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-0431-6_18
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DOI: https://doi.org/10.1007/978-94-009-0431-6_18
Publisher Name: Springer, Dordrecht
Print ISBN: 978-0-412-38560-5
Online ISBN: 978-94-009-0431-6
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