Guidance, Navigation, and Control Conference 1996
DOI: 10.2514/6.1996-3796
|View full text |Cite
|
Sign up to set email alerts
|

Input shaping for limiting loads and vibration in systems with on-off actuators

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
4
1

Citation Types

0
9
0

Year Published

1997
1997
2023
2023

Publication Types

Select...
7
1

Relationship

0
8

Authors

Journals

citations
Cited by 23 publications
(9 citation statements)
references
References 3 publications
0
9
0
Order By: Relevance
“…Such closed-form commands are also available for cases where the transient deflection 111,112 and the fuel usage 109,110 need to be limited. Another simple method for command shaping with on/off actuators is an approach where standard input-shaped commands are converted to an on/off function by approximation, 113,114 or pulse-width modulation. 115,116…”
Section: Input Shaping For Time-optimal Controlmentioning
confidence: 99%
“…Such closed-form commands are also available for cases where the transient deflection 111,112 and the fuel usage 109,110 need to be limited. Another simple method for command shaping with on/off actuators is an approach where standard input-shaped commands are converted to an on/off function by approximation, 113,114 or pulse-width modulation. 115,116…”
Section: Input Shaping For Time-optimal Controlmentioning
confidence: 99%
“…Some heuristic methods for extending input shaping to the case of on-off actuators have been developed. 19 Use of constraintson the impulse amplitudes have been used to generate a) Rotary system b) Linear system time-optimal command pro les for on-off reaction jets. Liu and Wie, 7 Singh and Vadali, 9 and Wie et al 20 demonstratedon-off input shapingwith mass, spring,and damper simulations.Singhoseet al 10 used a detailed nonlinear simulation of the Space Shuttle's remote manipulator and hardware experiments to demonstrate extra-robust input shaping for on-off actuators.…”
Section: Introductionmentioning
confidence: 99%
“…Flexible spacecraft equipped with on-off reaction jets cannot produce the variable-amplitude actuation force that is usually required with input shaping; the spacecraft must be moved with constant amplitude force pulses. Some heuristic methods for extending input shaping to the case of on-off actuators have been developed [11]. The use of constraint on the impulse amplitudes have been used to generate time-optimal command profiles for on-off reaction jets.…”
Section: Introductionmentioning
confidence: 99%