Optimal control theory with aerospace applications
I tiakina i:
| Kaituhi matua: | |
|---|---|
| Kaituhi rangatōpū: | |
| Hōputu: | Tāhiko īPukapuka |
| Reo: | Ingarihi |
| I whakaputaina: |
Reston, Va. :
American Institute of Aeronautics and Astronautics, Inc.,
c2010.
|
| Rangatū: | AIAA education series.
|
| Ngā marau: | |
| Urunga tuihono: | An electronic book accessible through the World Wide Web; click to view |
| Ngā Tūtohu: |
Tāpirihia he Tūtohu
Kāore He Tūtohu, Me noho koe te mea tuatahi ki te tūtohu i tēnei pūkete!
|
Rārangi ihirangi:
- Historical background
- Ordinary minimum problems : from the beginning of calculus to Kuhn-Tucker
- Calculus of variations : from Bernoulli to Bliss
- Minimum principle of Pontryagin and Hestenes
- Application of the Jacobi test in optimal control and neighboring extremals
- Numerical techniques for the optimal control problem
- Singular perturbation technique and its application to air-to-space interception
- Application to aircraft performance : Rutowski and Kaiser's techniques and more
- Application to rocket performance : the Goddard problem
- Application to missile guidance : proportional navigation
- Application to time-optimal rotational maneuvers of flexible spacecraft.