Summary of the digital adaptive filter, digital polynomial filter and specification set control techniques applied to large launch vehicles

Study on Digital Adaptive Flight Control of a Winged Rocket

下沢智啓

January 2012

九州工業大学博士学位論文学位記番号:工博甲第331号学位授与年月日:平成24年3月23日第1章緒論|第2章非最小位相特性を考慮したモデル規範形適応制御|第3章適応フィードバック線形化制御|第...

Analysis and design of space vehicle flight control systems. Volume VII - Attitude control during launch

Greensite, A. L.

July 1967

Analysis and design of space vehicle control systems - short period dynamics of attitude control dur...

NASA Marshall Space Flight Center Controls Systems Design and Analysis Branch

Gilligan, Eric

January 2014

Marshall Space Flight Center maintains a critical national capability in the analysis of launch vehi...

Control techniques for large launch vehicles Final report, Jul. 1964 - Sep. 1965

Luedde, W. J.
Zaborszky, J.

September 1965

Fuel sloshing and rigid body oscillations in large rocket booster control during launchin

Study of structural bending adaptive control techniques for large launch vehicles Technical summary report, volume I

March 1966

Application of spectral identification adaptive control system to large launch vehicle in complete c...

Space Launch System Ascent Flight Control Design

Wall, John H.
VanZwieten, Tannen S.
Orr, Jeb S.
Hall, Charles E.

January 2014

A robust and flexible autopilot architecture for NASA's Space Launch System (SLS) family of launch v...

Space Launch System Implementation of Adaptive Augmenting Control

VanZwieten, Tannen S.
Wall, John H.
Orr, Jeb S.

January 2014

Given the complex structural dynamics, challenging ascent performance requirements, and rigorous fli...

Digital adaptive flight controller development

Kaufman, H.
Alag, G.
Berry, P.
Kotob, S.

December 1974

A design study of adaptive control logic suitable for implementation in modern airborne digital flig...

Launch Vehicle Manual Steering with Adaptive Augmenting Control:In-Flight Evaluations of Adverse Interactions Using a Piloted Aircraft

Orr, Jeb S.
Miller, Chris
VanZwieten, Tannen S.
Gilligan, Eric T.
Wall, John H.
Hanson, Curt

January 2015

An Adaptive Augmenting Control (AAC) algorithm for the Space Launch System (SLS) has been developed ...

Some effects of digital sampling on orbiter flight control system operation

Murray, S. V.

January 1985

An entry dynamic stability ground test of the OV102 Space Shuttle Orbiter revealed some small amplit...

Space shuttle digital flight control system

Cox, K. J.
Minott, G. M.
Peller, J. B.

August 1976

The space shuttle digital, fly by wire, flight control system presents an interesting challenge in a...

A discussion of the stability requirements for a launch vehicle flight control system

Redus, J. R.

May 1968

Launch vehicle flight control system and relation to stability requirements and dynamic response

Analysis and design of space vehicle flight control systems. Volume IX - Optimization methods

Greensite, A. L.

July 1967

Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...

Development of a digital guidance and control law for steep approach automatic landings using modern control techniques

Halyo, N.

February 1979

The development of a digital automatic control law for a small jet transport to perform a steep fina...

Optimal control of a flexible launch vehicle Final report

Rynaski, E. G.
Wierwille, W. W.
Whitbeck, R. F.

July 1966

Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...

Study on Digital Adaptive Flight Control of a Winged Rocket

下沢智啓

January 2012

九州工業大学博士学位論文学位記番号:工博甲第331号学位授与年月日:平成24年3月23日第1章緒論|第2章非最小位相特性を考慮したモデル規範形適応制御|第3章適応フィードバック線形化制御|第...

Analysis and design of space vehicle flight control systems. Volume VII - Attitude control during launch

Greensite, A. L.

July 1967

Analysis and design of space vehicle control systems - short period dynamics of attitude control dur...

NASA Marshall Space Flight Center Controls Systems Design and Analysis Branch

Gilligan, Eric

January 2014

Marshall Space Flight Center maintains a critical national capability in the analysis of launch vehi...

Control techniques for large launch vehicles Final report, Jul. 1964 - Sep. 1965

Luedde, W. J.
Zaborszky, J.

September 1965

Fuel sloshing and rigid body oscillations in large rocket booster control during launchin

Study of structural bending adaptive control techniques for large launch vehicles Technical summary report, volume I

March 1966

Application of spectral identification adaptive control system to large launch vehicle in complete c...

Space Launch System Ascent Flight Control Design

Wall, John H.
VanZwieten, Tannen S.
Orr, Jeb S.
Hall, Charles E.

January 2014

A robust and flexible autopilot architecture for NASA's Space Launch System (SLS) family of launch v...

Space Launch System Implementation of Adaptive Augmenting Control

VanZwieten, Tannen S.
Wall, John H.
Orr, Jeb S.

January 2014

Given the complex structural dynamics, challenging ascent performance requirements, and rigorous fli...

Digital adaptive flight controller development

Kaufman, H.
Alag, G.
Berry, P.
Kotob, S.

December 1974

A design study of adaptive control logic suitable for implementation in modern airborne digital flig...

Launch Vehicle Manual Steering with Adaptive Augmenting Control:In-Flight Evaluations of Adverse Interactions Using a Piloted Aircraft

Orr, Jeb S.
Miller, Chris
VanZwieten, Tannen S.
Gilligan, Eric T.
Wall, John H.
Hanson, Curt

January 2015

An Adaptive Augmenting Control (AAC) algorithm for the Space Launch System (SLS) has been developed ...

Some effects of digital sampling on orbiter flight control system operation

Murray, S. V.

January 1985

An entry dynamic stability ground test of the OV102 Space Shuttle Orbiter revealed some small amplit...

Space shuttle digital flight control system

Cox, K. J.
Minott, G. M.
Peller, J. B.

August 1976

The space shuttle digital, fly by wire, flight control system presents an interesting challenge in a...

A discussion of the stability requirements for a launch vehicle flight control system

Redus, J. R.

May 1968

Launch vehicle flight control system and relation to stability requirements and dynamic response

Analysis and design of space vehicle flight control systems. Volume IX - Optimization methods

Greensite, A. L.

July 1967

Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...

Development of a digital guidance and control law for steep approach automatic landings using modern control techniques

Halyo, N.

February 1979

The development of a digital automatic control law for a small jet transport to perform a steep fina...

Optimal control of a flexible launch vehicle Final report

Rynaski, E. G.
Wierwille, W. W.
Whitbeck, R. F.

July 1966

Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...

Study on Digital Adaptive Flight Control of a Winged Rocket

下沢智啓

January 2012

九州工業大学博士学位論文学位記番号:工博甲第331号学位授与年月日:平成24年3月23日第1章緒論|第2章非最小位相特性を考慮したモデル規範形適応制御|第3章適応フィードバック線形化制御|第...

Analysis and design of space vehicle flight control systems. Volume VII - Attitude control during launch

Greensite, A. L.

July 1967

Analysis and design of space vehicle control systems - short period dynamics of attitude control dur...

NASA Marshall Space Flight Center Controls Systems Design and Analysis Branch

Gilligan, Eric

January 2014

Marshall Space Flight Center maintains a critical national capability in the analysis of launch vehi...

Summary of the digital adaptive filter, digital polynomial filter and specification set control techniques applied to large launch vehicles

Abstract

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Summary of the digital adaptive filter, digital polynomial filter and specification set control techniques applied to large launch vehicles

Abstract

Extracted data

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