Advances in Aerospace Guidance, Navigation and Control 2015
DOI: 10.1007/978-3-319-17518-8_27
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Integrated Design and Control of a Flying Wing Using Nonsmooth Optimization Techniques

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Cited by 5 publications
(10 citation statements)
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“…A single bandwidth and damping of, respectively, ω 0 8.8 rad ⋅ s −1 (1.4 Hz) and ξ 0.8 was used. Previous studies considered allocating different bandwidths for all control surfaces [14,39]; however, this is outside the scope of the present paper. A 100 ms delay accounting for sensors, computers, and data processing is included in the control law synthesis and simulation.…”
Section: Actuator Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…A single bandwidth and damping of, respectively, ω 0 8.8 rad ⋅ s −1 (1.4 Hz) and ξ 0.8 was used. Previous studies considered allocating different bandwidths for all control surfaces [14,39]; however, this is outside the scope of the present paper. A 100 ms delay accounting for sensors, computers, and data processing is included in the control law synthesis and simulation.…”
Section: Actuator Modelmentioning
confidence: 99%
“…Consequently, several approaches seek to solve these combined problems in a single step. "Plant-controller optimization" has been studied in a variety of fields, such as chemistry [19,20], autonomous underwater vehicles [21], and astronautics [14,22,23].…”
Section: Introductionmentioning
confidence: 99%
“…For some 0 < c 1 < c 2 < 1. Equation 14 ensures an improvement in the search when d is a descent direction. Note that Equation 14 will be satisfied for any small α because of Lemma 1, in which case the improvement may be limited.…”
Section: Optimality Conditionsmentioning
confidence: 99%
“…Equation 14 ensures an improvement in the search when d is a descent direction. Note that Equation 14 will be satisfied for any small α because of Lemma 1, in which case the improvement may be limited. Therefore, the curvature condition (15) is added to ensure that the chosen step length is not too conservative.…”
Section: Optimality Conditionsmentioning
confidence: 99%
“…One of the most notable examples are flying wings. By careful positioning of the center of gravity, it is possible to achieve static stability for these configurations as well, even though in most of the cases they require the presence of a stability augmentation system to ensure adequate flight characteristics [33][34][35].…”
Section: Horizontal Tailplane Designmentioning
confidence: 99%