Static aeroelastic optimisation to wing structural weight estimation of an extremely manoeuvrable UAV.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1218, p. 1033, doi. 10.1017/S0001924000004310
- By:
- Publication type:
- Article
Works matching IS 00019240 AND DT 2015 AND VI 119 AND IP 1218
Results: 6
1
2
Trajectory estimation based on extended state observer with Fal-filter.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1218, p. 1017, doi. 10.1017/S0001924000004309
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- Publication type:
- Article
3
Fixed-wing approach techniques for complex environments.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1218, p. 999, doi. 10.1017/S0001924000004292
- By:
- Publication type:
- Article
4
Weight functions method for stability analysis applied as design tool for Hawker 800XP aircraft.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1218, p. 981, doi. 10.1017/S0001924000004280
- By:
- Publication type:
- Article
5
Reduced order system identification for UAVs.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1218, p. 961, doi. 10.1017/S0001924000004279
- By:
- Publication type:
- Article
6
A technique to predict the aerodynamic effects of battle damage on an aircraft's wing.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1218, p. 937, doi. 10.1017/S0001924000004267
- By:
- Publication type:
- Article