Supervising Control for Unmanned Aerial Vehicles

Table 2

Formulae for calculation of stability derivatives.

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Longitudinal dimensional stability derivatives

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𝑋_𝑈=−𝑄𝑆(𝐶^𝑈_𝐷+2𝐶_𝐷0)/𝑀𝑢₀

𝑍_𝑈=−𝑄𝑆(𝐶^𝑈_𝐿+2𝐶_𝐿0)/𝑀𝑢₀

𝑍_𝛼=−𝑄𝑆(𝐶^𝛼_𝐿+2𝐶_𝐷0)/𝑀

𝑀_𝑈=𝑄𝑆𝐶(𝐶^𝑢_𝑚+2𝐶_𝑚0)/𝐼_𝑌𝑢₀

𝑀_𝛼=𝑄𝑆𝐶(𝐶^𝛼_𝑚)/𝐼_𝑌

𝑀_𝑞=𝑄𝑆𝐶𝐶(𝐶^𝑞_𝑚)/2𝐼_𝑌𝑢₀

𝑋_𝛿𝑒=−𝑄𝑆(𝐶_𝐷^𝛿𝑒)/𝑀

𝑍_𝛿𝑒=−𝑄𝑆(𝐶_𝐿^𝛿𝑒)/𝑀

𝑀_𝛿𝑒=𝑄𝑆𝐶(𝐶_𝑚^𝛿𝑒)/𝐼_𝑌

𝑍_̇𝛼=−𝑄𝑆𝐶(𝐶^̇𝛼_𝐿)/2𝑀𝑢₀

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