Table 7 Summary of the 30 constant parameters for the presented inverse simulation model.
Parameters group | Parameters symbols | Parameters count |
|---|---|---|
Airplane mass | \(m\) | 1 |
Wing planform (projected) area | \(S\) | 1 |
Mean aerodynamic chord (MAC) | \(c\) | 1 |
Wing span | \(b\) | 1 |
Mass moments and products of inertia about body axes | \(A, B, C, D, E, F\) | 6 |
Aerodynamic-force constants | \({C}_{L0},{C}_{L\alpha }, {C}_{D0},{K}_{CD}, {C}_{C\beta }\) | 5 |
Longitudinal stability derivatives | \({C}_{m0}, {C}_{m\alpha }, {C}_{mq}, {C}_{m\delta m}\) | 4 |
Lateral stability derivatives | \({C}_{l\beta }, {C}_{lp},{C}_{lr},{C}_{l\delta l},{C}_{l\delta n}\) | 5 |
Directional stability derivatives | \({C}_{n\beta }, {C}_{np}, {C}_{nr}, {C}_{n\delta l}, {C}_{n\delta n}\) | 5 |
Initial altitude | \({h}_{ini}\) | 1 |
Total | 30 | |
