| Nome |
# |
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Combining Global and Local Strategies to Optimize Parameters in Magnetic Spacecraft Control via Attitude Feedback, file e3835322-2127-15e8-e053-a505fe0a3de9
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185
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Lunar Ascent and Orbit Injection via Neighboring Optimal Guidance and Constrained Attitude Control, file e383531c-2973-15e8-e053-a505fe0a3de9
|
179
|
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A robust optimization approach for magnetic spacecraft attitude stabilization, file e3835319-ed83-15e8-e053-a505fe0a3de9
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159
|
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Variable-time-domain neighboring optimal guidance and attitude control of low-thrust lunar orbit transfers, file e3835325-67a2-15e8-e053-a505fe0a3de9
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152
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Determining optimal parameters in magnetic spacecraft stabilization via attitude feedback, file e383531a-3bdd-15e8-e053-a505fe0a3de9
|
121
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Neighboring optimal guidance and proportional-derivative attitude control applied to low-thrust orbit transfers, file e3835326-0fb5-15e8-e053-a505fe0a3de9
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102
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Quaternion versus Rotation Matrix Feedback for Spacecraft Attitude Stabilization Using Magnetorquers, file 7992ff80-77d6-41c0-b31e-d81f6a112975
|
97
|
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Global and robust attitude control of a launch vehicle in exoatmospheric flight, file e383531b-d41a-15e8-e053-a505fe0a3de9
|
97
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A new guidance and control architecture for accurate orbit injection, file e3835323-9cc5-15e8-e053-a505fe0a3de9
|
85
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Neighboring optimal guidance and attitude control of low-thrust earth orbit transfers, file e3835328-179d-15e8-e053-a505fe0a3de9
|
78
|
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Spacecraft attitude motion planning on SO(3) using gradient-based optimization: case studies, file e3835326-0fb4-15e8-e053-a505fe0a3de9
|
71
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|
Robust Collocated Control of Large Flexible Space Structures, file 6801977d-4adc-4616-ac81-267203e9adfd
|
57
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Robust three-axis attitude stabilization for inertial pointing spacecraft using magnetorquers, file e3835314-b7a6-15e8-e053-a505fe0a3de9
|
53
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Minimum-Time Spacecraft Attitude Motion Planning Using Objective Alternation in Derivative-Free Optimization, file e383532c-201a-15e8-e053-a505fe0a3de9
|
46
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|
Spacecraft attitude motion planning on SO(3) using gradient-based optimization, file e3835323-ccf9-15e8-e053-a505fe0a3de9
|
45
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|
Neighboring optimal guidance and constrained attitude control applied to three-dimensional lunar ascent and orbit injection, file e3835325-bbe2-15e8-e053-a505fe0a3de9
|
34
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|
Lunar descent and landing via two-phase explicit guidance and pulse-modulated reduced-attitude control, file a268e98d-dac3-46de-a536-094e8e8ea33a
|
31
|
|
Variable-time-domain neighboring optimal guidance and attitude control of low-thrust lunar orbit transfers, file e3835328-18e6-15e8-e053-a505fe0a3de9
|
28
|
|
Gain Selection for Attitude Stabilization of Earth-Pointing Spacecraft Using Magnetorquers, file 79ce23bb-721a-4454-8430-17b10648dd2e
|
16
|
|
Crane feedback control in offshore moonpool operations, file e3835325-f15b-15e8-e053-a505fe0a3de9
|
16
|
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Spacecraft attitude motion planning on SO(3) using gradient-based optimization: case studies, file e3835325-d4f3-15e8-e053-a505fe0a3de9
|
15
|
|
Neighboring optimal guidance and constrained attitude control for accurate orbit injection, file d4dc2328-e002-4318-945f-d5e91604ae00
|
13
|
|
Neighboring optimal guidance and proportional-derivative attitude control applied to low-thrust orbit transfers, file e3835325-d4f5-15e8-e053-a505fe0a3de9
|
12
|
|
Explicit near-optimal guidance and pulse-modulated control for lunar descent and touchdown, file 7e5303e0-e897-4e45-aff9-e38cdb0a928e
|
10
|
|
Global and robust attitude control of a launch vehicle in exoatmospheric flight, file e383531b-e8a9-15e8-e053-a505fe0a3de9
|
8
|
|
Spacecraft attitude motion planning using rotation matrices and gradient-based optimization, file c06f714c-4a8d-490c-8ceb-fa81a12ea6d1
|
7
|
|
Spacecraft attitude stabilization using magnetorquers with separation between measurement and actuation, file e3835314-b1f9-15e8-e053-a505fe0a3de9
|
5
|
|
Neighboring optimal guidance and constrained attitude control applied to three-dimensional lunar ascent and orbit injection, file e3835323-ab81-15e8-e053-a505fe0a3de9
|
5
|
|
Hybrid control for the pendubot, file e3835325-4651-15e8-e053-a505fe0a3de9
|
5
|
|
A reduction paradigm for output regulation, file e3835325-4659-15e8-e053-a505fe0a3de9
|
5
|
|
Robust three-axis attitude stabilization for inertial pointing spacecraft using magnetorquers, file e3835317-1971-15e8-e053-a505fe0a3de9
|
4
|
|
Gain selection for attitude stabilization of earth-pointing spacecraft using magnetorquers, file e383531b-4723-15e8-e053-a505fe0a3de9
|
4
|
|
Lunar descent and landing via two-phase explicit guidance and pulse-modulated reduced-attitude control, file 15191db5-8e58-4dba-983b-600194ff60dc
|
3
|
|
Correction to: Lunar Descent and Landing via Two-Phase Explicit Guidance and Pulse-Modulated Reduced-Attitude Control, file 49cc4dbf-b7ec-4641-a8cc-d82999346aaa
|
3
|
|
Discrete-time Sliding Mode controller for inverters, file e3835312-50ff-15e8-e053-a505fe0a3de9
|
3
|
|
A robust optimization approach for magnetic spacecraft attitude stabilization, file e383531a-662b-15e8-e053-a505fe0a3de9
|
3
|
|
Crane feedback control in offshore moonpool operations, file e3835325-4657-15e8-e053-a505fe0a3de9
|
3
|
|
Discrete-time control for DC-AC converters based on sliding mode design, file 5da2041c-06dc-49dc-9b1d-596ef008ac51
|
2
|
|
New implicit neighboring optimal guidance and attitude control for three-dimensional lunar ascent, file e3835319-c19f-15e8-e053-a505fe0a3de9
|
2
|
|
Neighboring optimal guidance and attitude control for lunar ascent and orbit injection, file e3835319-d2a8-15e8-e053-a505fe0a3de9
|
2
|
|
Spacecraft attitude motion planning using GRAFS, file e383531b-1aea-15e8-e053-a505fe0a3de9
|
2
|
|
Optimal feedback gains for spacecraft attitude stabilization using magnetorquers, file e383531b-e8ac-15e8-e053-a505fe0a3de9
|
2
|
|
Neighboring optimal guidance and attitude control of low-thrust earth orbit transfers, file e3835327-82d6-15e8-e053-a505fe0a3de9
|
2
|
|
Variable-time-domain neighboring optimal guidance and attitude control of low-thrust lunar orbit transfers, file e3835327-cc85-15e8-e053-a505fe0a3de9
|
2
|
|
Robust three-axis attitude stabilization for inertial pointing spacecraft using magnetorquers, file e3835329-d21c-15e8-e053-a505fe0a3de9
|
2
|
|
Explicit near-optimal guidance and pulse-modulated control for lunar descent and touchdown, file e383532c-c2de-15e8-e053-a505fe0a3de9
|
2
|
|
Certainty equivalence in nonlinear output regulation with unmeasured error, file f92356e4-d6fd-4f0a-9143-3644b02fba64
|
2
|
|
Spacecraft attitude motion planning using gradient-based optimization, file 830def4f-8978-4c69-9ad3-1436c64df4d6
|
1
|
|
A reduction paradigm for output regulation, file b0a15086-204a-4963-8d92-f50d67577f8a
|
1
|
|
Dead time generator for synchronous boost converters with GaN transistors, file e3835312-b614-15e8-e053-a505fe0a3de9
|
1
|
|
Magnetic spacecraft attitude stabilization via output feedback with separation between measurement and actuation., file e3835314-b79a-15e8-e053-a505fe0a3de9
|
1
|
|
Spacecraft attitude stabilization with piecewise-constant magnetic dipole moment, file e3835314-bc65-15e8-e053-a505fe0a3de9
|
1
|
|
Magnetic spacecraft control via output feedback with separation between measurement and actuation, file e383531b-4590-15e8-e053-a505fe0a3de9
|
1
|
|
Variable-time-domain neighboring optimal guidance and attitude control for low-thrust orbit transfers, file e383531b-4726-15e8-e053-a505fe0a3de9
|
1
|
|
Lunar Ascent and Orbit Injection via Neighboring Optimal Guidance and Constrained Attitude Control, file e383531c-5911-15e8-e053-a505fe0a3de9
|
1
|
|
Determining optimal parameters in magnetic spacecraft stabilization via attitude feedback, file e3835322-378d-15e8-e053-a505fe0a3de9
|
1
|
|
A Luenberger-style observer for robot manipulators with position measurements, file e3835325-6d34-15e8-e053-a505fe0a3de9
|
1
|
|
Crane feedback control in offshore moonpool operations, file e3835325-f15a-15e8-e053-a505fe0a3de9
|
1
|
|
Quaternion versus rotation matrix feedback for tigrisat attitude stabilization, file e383532c-f222-15e8-e053-a505fe0a3de9
|
1
|
|
Quaternion versus rotation matrix feedback for tigrisat attitude stabilization, file e383532c-f3d1-15e8-e053-a505fe0a3de9
|
1
|
| Totale |
1.793 |