Abstract
In this paper, the multiple-delay-model and multiple-design-point (MDM/MDP) approach is applied to the AIAA 1992 Controls Design Challenge. Design goals of the flight control system are presented with standard quadratic performance indices, and linear control laws of constant feedback gains are obtained numerically with parameter optimization. Robustness against uncertainties is guaranteed by giving appropriate MDMs, and robustness against changing dynamics is obtained by selecting MDPs. Trade-offs between control performance and robustness are conducted with MDMs. Simple Pis introduce reasonable feedback control laws. Realistic control laws are derived from the analytical results. Time responses of the two given flight missions and performances at four evaluation points demonstrate feasibility of the simple constant-gain feedback control.
| Original language | English |
|---|---|
| Pages (from-to) | 508-515 |
| Number of pages | 8 |
| Journal | Journal of Guidance, Control, and Dynamics |
| Volume | 18 |
| Issue number | 3 |
| DOIs | |
| Publication status | Published - 1995 |
| Externally published | Yes |
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All Science Journal Classification (ASJC) codes
- Control and Systems Engineering
- Aerospace Engineering
- Space and Planetary Science
- Applied Mathematics
- Electrical and Electronic Engineering
Cite this
Design with multiple-delay-model and multiple-design-point approach. / Miyazawa, Yoshikazu.
In: Journal of Guidance, Control, and Dynamics, Vol. 18, No. 3, 1995, p. 508-515.Research output: Contribution to journal › Article
}
TY - JOUR
T1 - Design with multiple-delay-model and multiple-design-point approach
AU - Miyazawa, Yoshikazu
PY - 1995
Y1 - 1995
N2 - In this paper, the multiple-delay-model and multiple-design-point (MDM/MDP) approach is applied to the AIAA 1992 Controls Design Challenge. Design goals of the flight control system are presented with standard quadratic performance indices, and linear control laws of constant feedback gains are obtained numerically with parameter optimization. Robustness against uncertainties is guaranteed by giving appropriate MDMs, and robustness against changing dynamics is obtained by selecting MDPs. Trade-offs between control performance and robustness are conducted with MDMs. Simple Pis introduce reasonable feedback control laws. Realistic control laws are derived from the analytical results. Time responses of the two given flight missions and performances at four evaluation points demonstrate feasibility of the simple constant-gain feedback control.
AB - In this paper, the multiple-delay-model and multiple-design-point (MDM/MDP) approach is applied to the AIAA 1992 Controls Design Challenge. Design goals of the flight control system are presented with standard quadratic performance indices, and linear control laws of constant feedback gains are obtained numerically with parameter optimization. Robustness against uncertainties is guaranteed by giving appropriate MDMs, and robustness against changing dynamics is obtained by selecting MDPs. Trade-offs between control performance and robustness are conducted with MDMs. Simple Pis introduce reasonable feedback control laws. Realistic control laws are derived from the analytical results. Time responses of the two given flight missions and performances at four evaluation points demonstrate feasibility of the simple constant-gain feedback control.
UR - http://www.scopus.com/inward/record.url?scp=85003340048&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85003340048&partnerID=8YFLogxK
U2 - 10.2514/3.21416
DO - 10.2514/3.21416
M3 - Article
VL - 18
SP - 508
EP - 515
JO - Journal of Guidance, Control, and Dynamics
JF - Journal of Guidance, Control, and Dynamics
SN - 0731-5090
IS - 3
ER -